Surgical instrument comprising a signal interference resolution system

ABSTRACT

A surgical instrument including a signal interference detection system.

CROSS-REFERENCE TO RELATED APPLICATION

The present application claims priority under 35 U.S.C. § 119(e) to U.S.Provisional Patent Application Ser. No. 62/955,306, entitled SURGICALINSTRUMENT SYSTEMS, filed Dec. 30, 2019, the disclosure of which isincorporated by reference in its entirety.

BACKGROUND

The present invention relates to surgical instruments and, in variousarrangements, to surgical stapling and cutting instruments and staplecartridges for use therewith that are designed to staple and cut tissue.

BRIEF DESCRIPTION OF THE DRAWINGS

Various features of the embodiments described herein, together withadvantages thereof, may be understood in accordance with the followingdescription taken in conjunction with the accompanying drawings asfollows:

FIG. 1 is a plan view of a surgical instrument assembly comprising ashaft, an end effector attached to the shaft, and a stretchable opticalwaveguide attached to the shaft and a firing member;

FIG. 2 is a partial perspective view of the surgical instrument assemblyof FIG. 1 illustrated with components removed;

FIG. 3 is a perspective view of a surgical instrument assemblycomprising the shaft and the end effector of FIG. 1 and a stretchableoptical waveguide attached to the shaft and a knife body;

FIG. 4 is an elevational view of a surgical instrument assemblycomprising the shaft and the end effector of FIG. 1 and a stretchableoptical waveguide attached to the end effector and the knife body,wherein the knife body is illustrated in a home position;

FIG. 5 is an elevational view of the surgical instrument assembly ofFIG. 4, wherein the knife body is illustrated in an end-of-strokeposition;

FIG. 6 is an elevational view of the surgical instrument assembly ofFIG. 4, wherein the end effector is articulated relative to the shaft;

FIG. 7A is a partial perspective view of a surgical instrument assemblycomprising a shaft, an actuation member, and a sensing system configuredto sense a parameter of the actuation member;

FIG. 7B is an end view of the surgical instrument assembly of FIG. 7A;

FIG. 8 is a partial elevational view of a surgical instrument assemblycomprising a shaft, an actuation member, and a sensing system comprisingHall effect sensors configured to detect the position of the actuationmember;

FIG. 9 is graph of the position of the actuation member of FIG. 8relative to a motor position;

FIG. 10 is a graph of an expected voltage of the Hall effect sensors ofFIG. 8 relative to the motor position;

FIG. 11 is a graph including the graphs of FIGS. 9 and 10 and an exampleof an actual readout of the Hall effect sensors of FIG. 8 during anactuation stroke;

FIG. 12 is a graph of an actuation stroke of an actuation membermeasured by a motor encoder and a graph of the actuation stroke of theactuation member measured by a stretchable optical waveguide;

FIG. 13 is a partial perspective view of a surgical instrument assemblycomprising a shaft, an end effector attached to the shaft by way of anarticulation joint, and a flex circuit comprising a stretchable zone anda non-stretchable zone;

FIG. 14 is an elevational view of a stretchable zone of the flex circuitof FIG. 13 in a non-stretched configuration;

FIG. 15 is an elevational view of a stretchable zone of the flex circuitof FIG. 13 in a stretched configuration;

FIG. 16 is an elevational view of a flex circuit comprising astretchable zone comprising elastic strut members, wherein thestretchable zone is illustrated in a non-stretched configuration;

FIG. 17 is an elevational view of the flex circuit of FIG. 16, whereinthe stretchable zone is illustrated in a stretched configuration;

FIG. 18 is an elevational view of the flex circuit of FIG. 16, whereinthe stretchable zone is illustrated in a non-stretched configuration;

FIG. 19 is a perspective view of a surgical instrument assembly,illustrated with components removed, comprising a shaft and a flexcircuit extending through the shaft, wherein the flex circuit comprisesa pre-bent section;

FIG. 20 is a cross-sectional view of the flex circuit of FIG. 19;

FIG. 21 is a perspective view of a surgical instrument assembly,illustrated with components removed, comprising a shaft and a flexcircuit extending through the shaft, wherein the flex circuit comprisesa pre-bent section;

FIG. 22 is a cross-sectional view of the flex circuit of FIG. 21;

FIG. 23 is a perspective view of a surgical instrument assembly,illustrated with components removed, comprising a shaft and a flexcircuit extending through the shaft, wherein the flex circuit comprisesa pre-bent section;

FIG. 24 is a cross-sectional view of the flex circuit of FIG. 23;

FIG. 25 is a plan view of a surgical instrument assembly, illustratedwith components removed, comprising an articulation joint and a flexcircuit extending through the articulation joint, wherein the surgicalinstrument assembly is illustrated in a first articulated configuration;

FIG. 26 is a plan view of the surgical instrument assembly of FIG. 25,wherein the surgical instrument assembly is illustrated in a secondarticulated configuration;

FIG. 27 is a plan view of the surgical instrument assembly of FIG. 25,wherein the surgical instrument assembly is illustrated in anon-articulated configuration;

FIG. 28 is an elevational view of a surgical instrument assembly,illustrated with components removed, comprising an end effector, afiring member, and a sensing system comprising a plurality of sensorsand a magnet;

FIG. 29 is a plan view of the surgical instrument assembly of FIG. 28,wherein the firing member is in an unfired position;

FIG. 30 is a plan view of the surgical instrument assembly of FIG. 28,wherein the firing member is in a fired position;

FIG. 31 is a perspective view of a surgical instrument assembly,illustrated with components removed, comprising an end effector jawcomprising a staple cartridge channel configured to receive a staplecartridge therein and a sensing system comprising a plurality ofpressure sensors;

FIG. 32 is a cross-sectional view of the surgical instrument assembly ofFIG. 31 illustrating a staple cartridge positioned within the endeffector jaw;

FIG. 33 is a cross-sectional view of the surgical instrument assembly ofFIG. 31 illustrating a staple cartridge positioned within the endeffector jaw;

FIG. 34 is a perspective view of a surgical instrument assemblycomprising a handle, a shaft extending from the handle, an end effectorextending from the shaft, and a flex circuit extending through the shaftand comprising a sensing system,

FIG. 35 is a partial elevational view of the surgical instrumentassembly of FIG. 34, wherein an actuation member configured to be sensedby the sensing system comprises a first length;

FIG. 36 is a partial elevational view of the surgical instrumentassembly of FIG. 34, wherein the actuation member is under a load andcomprises a second length different than the first length of FIG. 35;

FIG. 37 is a partial exploded view of the surgical instrument assemblyof FIG. 34;

FIG. 38 is a plan view of a surgical instrument assembly, illustratedwith components removed, comprising a shaft, an articulation joint, anend effector attached to the shaft by way of the articulation joint, anda sensing system, wherein the surgical instrument assembly is in a firstarticulated configuration;

FIG. 39 is a plan view of the surgical instrument assembly of FIG. 38,wherein the surgical instrument assembly is in a second articulatedconfiguration;

FIG. 40 is a plan view of the surgical instrument assembly of FIG. 38,wherein the surgical instrument assembly is in a non-articulatedconfiguration;

FIG. 41 is a perspective view of a stretchable sensing fabric comprisinga body portion and a plurality of sensing materials positioned withinthe body portion;

FIG. 42 is a plan view of the stretchable sensing fabric of FIG. 41,wherein the stretchable sensing fabric is in a relaxed configuration;

FIG. 43 is a plan view of the stretchable sensing fabric of FIG. 41,wherein the stretchable sensing fabric is in a stretched configuration;

FIG. 44 is a perspective view of a surgical instrument assembly,illustrated with components removed, comprising a firing member and aplurality of the stretchable sensing fabric of FIG. 41;

FIG. 45 is a cross-sectional view of the surgical instrument assembly ofFIG. 44;

FIG. 46 is a perspective view of a surgical instrument assembly,illustrated with components removed, comprising a shaft, an end effectorattached to the shaft by way of an articulation joint, and a sensingsystem comprising a stretchable sensing fabric and a flex circuit;

FIG. 47 is a cross-sectional view of components of the surgicalinstrument assembly of FIG. 46;

FIG. 48 is a graph illustrating three different possible load profilesdefining a range of acceptable load profiles of an actuation member of asurgical instrument assembly;

FIG. 49 is a graph illustrating an actual load profile of an actuationmember compared to the range of acceptable load profiles defined in thegraph of FIG. 48;

FIG. 50 is a partial cross-sectional view of a surgical instrumentassembly, illustrated with components removed, comprising a sensingsystem configured to measure a parameter of the surgical instrumentassembly;

FIG. 51 is a plan view of the surgical instrument assembly of FIGS.28-30;

FIG. 52 comprises multiple graphs depicting sensor readings and datastream bandwidth of the sensing system of the surgical instrumentassembly of FIG. 51 relative to a firing stroke;

FIG. 53 is a perspective view of a surgical system comprising a surgicalinstrument attachment interface and a plurality of surgical instrumentattachments;

FIG. 54 is a partial perspective view of a surgical instrument assemblyoriented in an upright orientation;

FIG. 55 is a partial perspective view of the surgical instrumentassembly of FIG. 54 in an inverted orientation;

FIG. 56 is an elevational view of an end effector assembly comprising ananvil jaw and a cartridge jaw, wherein the end effector assembly isoriented in a direction where the anvil is opened in a direction whichcooperates with gravity;

FIG. 57 is an elevational view of the end effector assembly of FIG. 56,wherein the end effector is oriented in a direction where the anvil isopened in a direction which opposes gravity;

FIG. 58 is a partial exploded perspective view of a surgical instrumentassembly comprising an attachment interface, a shaft assembly attachableto the attachment interface, and a sensing system configured to detectthe orientation of the shaft assembly relative to the attachmentinterface;

FIG. 59 is a schematic representation of the sensing system of FIG. 58,wherein the shaft assembly is oriented in a first orientation;

FIG. 60 is a schematic representation of the sensing system of FIG. 58,wherein the shaft assembly is oriented in a second orientation;

FIG. 61 is a schematic representation of the sensing system of FIG. 58,wherein the shaft assembly is oriented in a third orientation;

FIG. 62 is an elevational view of an operating table and patient,wherein the operating table an patient are oriented in a firstorientation;

FIG. 63 is an elevational view of the operating table and patient ofFIG. 62, wherein the operating table an patient are oriented in a secondorientation;

FIG. 64 is an elevational view of the operating table and patient ofFIG. 62, wherein the operating table an patient are oriented in a thirdorientation;

FIG. 65 is a flow chart depicting a surgical instrument control circuit;and

FIG. 66 is a schematic of a surgical instrument system comprising a huband a plurality of modular instrument assemblies.

Corresponding reference characters indicate corresponding partsthroughout the several views. The exemplifications set out hereinillustrate certain embodiments of the invention, in one form, and suchexemplifications are not to be construed as limiting the scope of theinvention in any manner.

DETAILED DESCRIPTION

Applicant of the present application owns the following U.S. PatentApplications that were filed on even date herewith, and which are eachherein incorporated by reference in their respective entireties:

-   -   Attorney Docket No. END9235USNP1/190718-1M, entitled METHOD FOR        OPERATING A SURGICAL INSTRUMENT;    -   Attorney Docket No. END9235USNP2/190718-2, entitled SURGICAL        INSTRUMENT COMPRISING AN ADJUSTMENT SYSTEM;    -   Attorney Docket No. END9235USNP3/190718-3, entitled SURGICAL        INSTRUMENT COMPRISING A CONTROL SYSTEM RESPONSIVE TO SOFTWARE        CONFIGURATIONS;    -   Attorney Docket No. END9235USNP4/190718-4, entitled SURGICAL        INSTRUMENT COMPRISING AN ORIENTATION DETECTION SYSTEM;    -   Attorney Docket No. END9235USNP6/190718-6, entitled SURGICAL        INSTRUMENT COMPRISING A FEEDBACK CONTROL CIRCUIT;    -   Attorney Docket No. END9235USNP7/190718-7, entitled SURGICAL        INSTRUMENT COMPRISING A FLEX CIRCUIT;    -   Attorney Docket No. END9235USNP8/190718-8, entitled SURGICAL        INSTRUMENT COMPRISING A SENSING SYSTEM; and    -   Attorney Docket No. END9235USNP9/190718-9, entitled SURGICAL        INSTRUMENT COMPRISING A FLEX CIRCUIT INCLUDING A SENSOR SYSTEM.

Applicant of the present application owns the following U.S. PatentApplications that were filed on May 29, 2020, and which are each hereinincorporated by reference in their respective entireties:

-   -   U.S. patent application Ser. No. 16/887,499, entitled USER        INTERFACE FOR SURGICAL INSTRUMENT WITH COMBINATION ENERGY        MODALITY END-EFFECTOR;    -   U.S. patent application Ser. No. 16/887,493, entitled METHOD OF        OPERATING A COMBINATION ULTRASONIC/BIPOLAR RF SURGICAL DEVICE        WITH A COMBINATION ENERGY MODALITY END-EFFECTOR;    -   U.S. patent application Ser. No. 16/887,506, entitled        DEFLECTABLE SUPPORT OF RF ENERGY ELECTRODE WITH RESPECT TO        OPPOSING ULTRASONIC BLADE;    -   U.S. patent application Ser. No. 16/887,515, entitled NON-BIASED        DEFLECTABLE ELECTRODE TO MINIMIZE CONTACT BETWEEN ULTRASONIC        BLADE AND ELECTRODE;    -   U.S. patent application Ser. No. 16/887,519, entitled        DEFLECTABLE ELECTRODE WITH HIGHER DISTAL BIAS RELATIVE TO        PROXIMAL BIAS;    -   U.S. patent application Ser. No. 16/887,532, entitled        DEFLECTABLE ELECTRODE WITH VARIABLE COMPRESSION BIAS ALONG THE        LENGTH OF THE DEFLECTABLE ELECTRODE;    -   U.S. patent application Ser. No. 16/887,554, entitled ASYMMETRIC        SEGMENTED ULTRASONIC SUPPORT PAD FOR COOPERATIVE ENGAGEMENT WITH        A MOVABLE RF ELECTRODE;    -   U.S. patent application Ser. No. 16/887,561, entitled VARIATION        IN ELECTRODE PARAMETERS AND DEFLECTABLE ELECTRODE TO MODIFY        ENERGY DENSITY AND TISSUE INTERACTION;    -   U.S. patent application Ser. No. 16/887,568, entitled TECHNIQUES        FOR DETECTING ULTRASONIC BLADE TO ELECTRODE CONTACT AND REDUCING        POWER TO ULTRASONIC BLADE;    -   U.S. patent application Ser. No. 16/887,576, entitled CLAMP ARM        JAW TO MINIMIZE TISSUE STICKING AND IMPROVE TISSUE CONTROL; and    -   U.S. patent application Ser. No. 16/887,579, entitled PARTIALLY        CONDUCTIVE CLAMP ARM PAD TO ENABLE ELECTRODE WEAR THROUGH AND        MINIMIZE SHORT CIRCUITING.

Applicant of the present application owns the following U.S. PatentApplications that were filed on May 28, 2020, and which are each hereinincorporated by reference in their respective entireties:

-   -   U.S. patent application Ser. No. 16/885,813, entitled METHOD FOR        AN ELECTROSURGICAL PROCEDURE;    -   U.S. patent application Ser. No. 16/885,820, entitled        ARTICULATABLE SURGICAL INSTRUMENT;    -   U.S. patent application Ser. No. 16/885,823, entitled SURGICAL        INSTRUMENT WITH JAW ALIGNMENT FEATURES;    -   U.S. patent application Ser. No. 16/885,826, entitled SURGICAL        INSTRUMENT WITH ROTATABLE AND ARTICULATABLE SURGICAL END        EFFECTOR;    -   U.S. patent application Ser. No. 16/885,838, entitled        ELECTROSURGICAL INSTRUMENT WITH ASYNCHRONOUS ENERGIZING        ELECTRODES;    -   U.S. patent application Ser. No. 16/885,851, entitled        ELECTROSURGICAL INSTRUMENT WITH ELECTRODES BIASING SUPPORT;    -   U.S. patent application Ser. No. 16/885,860, entitled        ELECTROSURGICAL INSTRUMENT WITH FLEXIBLE WIRING ASSEMBLIES;    -   U.S. patent application Ser. No. 16/885,866, entitled        ELECTROSURGICAL INSTRUMENT WITH VARIABLE CONTROL MECHANISMS;    -   U.S. patent application Ser. No. 16/885,870, entitled        ELECTROSURGICAL SYSTEMS WITH INTEGRATED AND EXTERNAL POWER        SOURCES;    -   U.S. patent application Ser. No. 16/885,873, entitled        ELECTROSURGICAL INSTRUMENTS WITH ELECTRODES HAVING ENERGY        FOCUSING FEATURES;    -   U.S. patent application Ser. No. 16/885,879, entitled        ELECTROSURGICAL INSTRUMENTS WITH ELECTRODES HAVING VARIABLE        ENERGY DENSITIES;    -   U.S. patent application Ser. No. 16/885,881, entitled        ELECTROSURGICAL INSTRUMENT WITH MONOPOLAR AND BIPOLAR ENERGY        CAPABILITIES;    -   U.S. patent application Ser. No. 16/885,888, entitled        ELECTROSURGICAL END EFFECTORS WITH THERMALLY INSULATIVE AND        THERMALLY CONDUCTIVE PORTIONS;    -   U.S. patent application Ser. No. 16/885,893, entitled        ELECTROSURGICAL INSTRUMENT WITH ELECTRODES OPERABLE IN BIPOLAR        AND MONOPOLAR MODES;    -   U.S. patent application Ser. No. 16/885,900, entitled        ELECTROSURGICAL INSTRUMENT FOR DELIVERING BLENDED ENERGY        MODALITIES TO TISSUE;    -   U.S. patent application Ser. No. 16/885,917, entitled CONTROL        PROGRAM ADAPTATION BASED ON DEVICE STATUS AND USER INPUT;    -   U.S. patent application Ser. No. 16/885,923, entitled CONTROL        PROGRAM FOR MODULAR COMBINATION ENERGY DEVICE; and    -   U.S. patent application Ser. No. 16/885,931, entitled SURGICAL        SYSTEM COMMUNICATION PATHWAYS.

Applicant of the present application owns the following U.S. ProvisionalPatent Applications that were filed on Dec. 30, 2019 and which are eachincorporated by reference in their respective entireties:

-   -   U.S. Provisional Patent Application Ser. No. 62/955,294,        entitled USER INTERFACE FOR SURGICAL INSTRUMENT WITH COMBINATION        ENERGY MODALITY END-EFFECTOR;    -   U.S. Provisional Patent Application Ser. No. 62/955,292,        entitled COMBINATION ENERGY MODALITY END-EFFECTOR; and    -   U.S. Provisional Patent Application Ser. No. 62/955,299,        entitled ELECTROSURGICAL INSTRUMENTS FOR COMBINATION ENERGY        DELIVERY.

Applicant of the present application owns the following U.S. PatentApplications that were filed on Dec. 19, 2019 and which are eachincorporated by reference in their respective entireties:

-   -   U.S. patent application Ser. No. 16/720,766, entitled METHOD FOR        OPERATING A SURGICAL INSTRUMENT;    -   U.S. patent application Ser. No. 16/720,706, entitled STAPLE        CARTRIDGE COMPRISING A SEATING CAM;    -   U.S. patent application Ser. No. 16/720,731, entitled SURGICAL        INSTRUMENT COMPRISING A RAPID CLOSURE MECHANISM;    -   U.S. patent application Ser. No. 16/720,735, entitled SURGICAL        INSTRUMENT COMPRISING A CLOSURE SYSTEM INCLUDING A CLOSURE        MEMBER AND AN OPENING MEMBER DRIVEN BY A DRIVE SCREW;    -   U.S. patent application Ser. No. 16/720,747, entitled SURGICAL        INSTRUMENT COMPRISING A NESTED FIRING MEMBER;    -   U.S. patent application Ser. No. 16/720,751, entitled STAPLE        CARTRIDGE COMPRISING A DEPLOYABLE KNIFE;    -   U.S. patent application Ser. No. 16/720,769, entitled STAPLE        CARTRIDGE COMPRISING A DETACHABLE TISSUE CUTTING KNIFE;    -   U.S. patent application Ser. No. 16/720,730, entitled STAPLING        SYSTEM COMPRISING A CLAMP LOCKOUT AND A FIRING LOCKOUT;    -   U.S. patent application Ser. No. 16/720,742, entitled STAPLE        CARTRIDGE COMPRISING A LATCH LOCKOUT;    -   U.S. patent application Ser. No. 16/720,776, entitled SURGICAL        INSTRUMENT COMPRISING A POWERED ARTICULATION SYSTEM;    -   U.S. patent application Ser. No. 16/720,781, entitled MOTOR        DRIVEN SURGICAL INSTRUMENT;    -   U.S. patent application Ser. No. 16/720,789, entitled STAPLING        INSTRUMENT COMPRISING INDEPENDENT JAW CLOSING AND STAPLE FIRING        SYSTEMS;    -   U.S. patent application Ser. No. 16/720,725, entitled STAPLE        CARTRIDGE COMPRISING DRIVER RETENTION MEMBERS;    -   U.S. patent application Ser. No. 16/720,740, entitled STAPLE        CARTRIDGE COMPRISING DRIVER RETENTION MEMBERS;    -   U.S. patent application Ser. No. 16/720,788, entitled STAPLE        CARTRIDGE COMPRISING PROJECTIONS EXTENDING FROM A CURVED DECK        SURFACE; and    -   U.S. patent application Ser. No. 16/720,806, entitled STAPLE        CARTRIDGE COMPRISING A CURVED DECK SURFACE.

Applicant of the present application owns the following U.S. PatentApplications that were filed on Sep. 5, 2019 and which are each hereinincorporated by reference in their respective entireties:

-   -   U.S. patent application Ser. No. 16/562,123, entitled METHOD FOR        CONSTRUCTING AND USING A MODULAR SURGICAL ENERGY SYSTEM WITH        MULTIPLE DEVICES;    -   U.S. patent application Ser. No. 16/562,135, entitled METHOD FOR        CONTROLLING AN ENERGY MODULE OUTPUT;    -   U.S. patent application Ser. No. 16/562,144, entitled METHOD FOR        CONTROLLING A MODULAR ENERGY SYSTEM USER INTERFACE; and    -   U.S. patent application Ser. No. 16/562,125, entitled METHOD FOR        COMMUNICATING BETWEEN MODULES AND DEVICES IN A MODULAR SURGICAL        SYSTEM.

Applicant of the present application owns the following U.S. PatentApplications that were filed on Mar. 25, 2019 and which are each hereinincorporated by reference in their respective entireties:

-   -   U.S. patent application Ser. No. 16/363,070, entitled FIRING        DRIVE ARRANGEMENTS FOR SURGICAL SYSTEMS;    -   U.S. patent application Ser. No. 16/363,051, entitled FIRING        DRIVE ARRANGEMENTS FOR SURGICAL SYSTEMS;    -   U.S. patent application Ser. No. 16/363,045, entitled        ARTICULATION DRIVE ARRANGEMENTS FOR SURGICAL SYSTEMS; and    -   U.S. patent application Ser. No. 16/363,062, entitled FIRING        DRIVE ARRANGEMENTS FOR SURGICAL SYSTEMS.

Applicant of the present application owns the following U.S. PatentApplications that were filed on Jun. 30, 2019 and which are each hereinincorporated by reference in their respective entireties:

-   -   U.S. patent application Ser. No. 16/458,104, entitled METHOD FOR        AUTHENTICATING THE COMPATIBILITY OF A STAPLE CARTRIDGE WITH A        SURGICAL INSTRUMENT;    -   U.S. patent application Ser. No. 16/458,108, entitled SURGICAL        INSTRUMENT SYSTEM COMPRISING AN RFID SYSTEM;    -   U.S. patent application Ser. No. 16/458,111, entitled SURGICAL        INSTRUMENT COMPRISING AN RFID SYSTEM FOR TRACKING A MOVABLE        COMPONENT;    -   U.S. patent application Ser. No. 16/458,114, entitled SURGICAL        INSTRUMENT COMPRISING AN ALIGNED RFID SENSOR;    -   U.S. patent application Ser. No. 16/458,105, entitled SURGICAL        STAPLING SYSTEM HAVING AN INFORMATION DECRYPTION PROTOCOL;    -   U.S. patent application Ser. No. 16/458,110, entitled SURGICAL        STAPLING SYSTEM HAVING AN INFORMATION ENCRYPTION PROTOCOL;    -   U.S. patent application Ser. No. 16/458,120, entitled SURGICAL        STAPLING SYSTEM HAVING A LOCKOUT MECHANISM FOR AN INCOMPATIBLE        CARTRIDGE;    -   U.S. patent application Ser. No. 16/458,125, entitled SURGICAL        STAPLING SYSTEM HAVING A FRANGIBLE RFID TAG; and    -   U.S. patent application Ser. No. 16/458,103, entitled PACKAGING        FOR A REPLACEABLE COMPONENT OF A SURGICAL STAPLING SYSTEM.

Applicant of the present application owns the following U.S. PatentApplications that were filed on Jun. 30, 2019 and which are each hereinincorporated by reference in their respective entireties:

-   -   U.S. patent application Ser. No. 16/458,107, entitled METHOD OF        USING MULTIPLE RFID CHIPS WITH A SURGICAL ASSEMBLY;    -   U.S. patent application Ser. No. 16/458,109, entitled MECHANISMS        FOR PROPER ANVIL ATTACHMENT SURGICAL STAPLING HEAD ASSEMBLY;    -   U.S. patent application Ser. No. 16/458,119, entitled MECHANISMS        FOR MOTOR CONTROL ADJUSTMENTS OF A MOTORIZED SURGICAL        INSTRUMENT;    -   U.S. patent application Ser. No. 16/458,115, entitled SURGICAL        INSTRUMENT WITH BATTERY COMPATIBILITY VERIFICATION        FUNCTIONALITY;    -   U.S. patent application Ser. No. 16/458,117, entitled SURGICAL        SYSTEM WITH RFID TAGS FOR UPDATING MOTOR ASSEMBLY PARAMETERS;    -   U.S. patent application Ser. No. 16/458,121, entitled SURGICAL        SYSTEMS WITH MULTIPLE RFID TAGS;    -   U.S. patent application Ser. No. 16/458,122, entitled RFID        IDENTIFICATION SYSTEMS FOR SURGICAL INSTRUMENTS;    -   U.S. patent application Ser. No. 16/458,106, entitled RFID        IDENTIFICATION SYSTEMS FOR SURGICAL INSTRUMENTS;    -   U.S. patent application Ser. No. 16/458,112, entitled SURGICAL        RFID ASSEMBLIES FOR DISPLAY AND COMMUNICATION;    -   U.S. patent application Ser. No. 16/458,116, entitled SURGICAL        RFID ASSEMBLIES FOR COMPATIBILITY DETECTION; and    -   U.S. patent application Ser. No. 16/458,118, entitled SURGICAL        RFID ASSEMBLIES FOR INSTRUMENT OPERATIONAL SETTING CONTROL.

Applicant of the present application owns the following U.S. PatentApplications, filed on Dec. 4, 2018, the disclosure of each of which isherein incorporated by reference in its entirety:

-   -   U.S. patent application Ser. No. 16/209,385, entitled METHOD OF        HUB COMMUNICATION, PROCESSING, STORAGE AND DISPLAY;    -   U.S. patent application Ser. No. 16/209,395, entitled METHOD OF        HUB COMMUNICATION;    -   U.S. patent application Ser. No. 16/209,403, entitled METHOD OF        CLOUD BASED DATA ANALYTICS FOR USE WITH THE HUB;    -   U.S. patent application Ser. No. 16/209,407, entitled METHOD OF        ROBOTIC HUB COMMUNICATION, DETECTION, AND CONTROL;    -   U.S. patent application Ser. No. 16/209,416, entitled METHOD OF        HUB COMMUNICATION, PROCESSING, DISPLAY, AND CLOUD ANALYTICS;    -   U.S. patent application Ser. No. 16/209,423, entitled METHOD OF        COMPRESSING TISSUE WITHIN A STAPLING DEVICE AND SIMULTANEOUSLY        DISPLAYING THE LOCATION OF THE TISSUE WITHIN THE JAWS;    -   U.S. patent application Ser. No. 16/209,427, entitled METHOD OF        USING REINFORCED FLEXIBLE CIRCUITS WITH MULTIPLE SENSORS TO        OPTIMIZE PERFORMANCE OF RADIO FREQUENCY DEVICES;    -   U.S. patent application Ser. No. 16/209,433, entitled METHOD OF        SENSING PARTICULATE FROM SMOKE EVACUATED FROM A PATIENT,        ADJUSTING THE PUMP SPEED BASED ON THE SENSED INFORMATION, AND        COMMUNICATING THE FUNCTIONAL PARAMETERS OF THE SYSTEM TO THE        HUB;    -   U.S. patent application Ser. No. 16/209,447, entitled METHOD FOR        SMOKE EVACUATION FOR SURGICAL HUB;    -   U.S. patent application Ser. No. 16/209,453, entitled METHOD FOR        CONTROLLING SMART ENERGY DEVICES;    -   U.S. patent application Ser. No. 16/209,458, entitled METHOD FOR        SMART ENERGY DEVICE INFRASTRUCTURE;    -   U.S. patent application Ser. No. 16/209,465, entitled METHOD FOR        ADAPTIVE CONTROL SCHEMES FOR SURGICAL NETWORK CONTROL AND        INTERACTION;    -   U.S. patent application Ser. No. 16/209,478, entitled METHOD FOR        SITUATIONAL AWARENESS FOR SURGICAL NETWORK OR SURGICAL NETWORK        CONNECTED DEVICE CAPABLE OF ADJUSTING FUNCTION BASED ON A SENSED        SITUATION OR USAGE;    -   U.S. patent application Ser. No. 16/209,490, entitled METHOD FOR        FACILITY DATA COLLECTION AND INTERPRETATION; and    -   U.S. patent application Ser. No. 16/209,491, entitled METHOD FOR        CIRCULAR STAPLER CONTROL ALGORITHM ADJUSTMENT BASED ON        SITUATIONAL AWARENESS.

Applicant of the present application owns the following U.S. PatentApplications that were filed on Jun. 26, 2019 and which are each hereinincorporated by reference in their respective entireties:

-   -   U.S. patent application Ser. No. 16/453,273, entitled METHOD FOR        PROVIDING AN AUTHENTICATION LOCKOUT IN A SURGICAL STAPLER WITH A        REPLACEABLE CARTRIDGE;    -   U.S. patent application Ser. No. 16/453,283, entitled SURGICAL        STAPLING ASSEMBLY WITH CARTRIDGE BASED RETAINER CONFIGURED TO        UNLOCK A FIRING LOCKOUT;    -   U.S. patent application Ser. No. 16/453,289, entitled SURGICAL        STAPLING ASSEMBLY WITH CARTRIDGE BASED RETAINER CONFIGURED TO        UNLOCK A CLOSURE LOCKOUT;    -   U.S. patent application Ser. No. 16/453,302 entitled UNIVERSAL        CARTRIDGE BASED KEY FEATURE THAT UNLOCKS MULTIPLE LOCKOUT        ARRANGEMENTS IN DIFFERENT SURGICAL STAPLERS;    -   U.S. patent application Ser. No. 16/453,310, entitled STAPLE        CARTRIDGE RETAINERS WITH FRANGIBLE RETENTION FEATURES AND        METHODS OF USING SAME;    -   U.S. patent application Ser. No. 16/453,330, entitled STAPLE        CARTRIDGE RETAINER WITH FRANGIBLE AUTHENTICATION KEY;    -   U.S. patent application Ser. No. 16/453,335, entitled STAPLE        CARTRIDGE RETAINER WITH RETRACTABLE AUTHENTICATION KEY;    -   U.S. patent application Ser. No. 16/453,343, entitled STAPLE        CARTRIDGE RETAINER SYSTEM WITH AUTHENTICATION KEYS;    -   U.S. patent application Ser. No. 16/453,355, entitled INSERTABLE        DEACTIVATOR ELEMENT FOR SURGICAL STAPLER LOCKOUTS;    -   U.S. patent application Ser. No. 16/453,369, entitled DUAL CAM        CARTRIDGE BASED FEATURE FOR UNLOCKING A SURGICAL STAPLER        LOCKOUT;    -   U.S. patent application Ser. No. 16/453,391, entitled STAPLE        CARTRIDGES WITH CAM SURFACES CONFIGURED TO ENGAGE PRIMARY AND        SECONDARY PORTIONS OF A LOCKOUT OF A SURGICAL STAPLING DEVICE;    -   U.S. patent application Ser. No. 16/453,413, entitled SURGICAL        STAPLE CARTRIDGES WITH MOVABLE AUTHENTICATION KEY ARRANGEMENTS;    -   U.S. patent application Ser. No. 16/453,423, entitled        DEACTIVATOR ELEMENT FOR DEFEATING SURGICAL STAPLING DEVICE        LOCKOUTS; and    -   U.S. patent application Ser. No. 16/453,429 entitled SURGICAL        STAPLE CARTRIDGES WITH INTEGRAL AUTHENTICATION KEYS.

Applicant of the present application owns the following U.S. DesignPatent Applications that were filed on Jun. 25, 2019 which are eachherein incorporated by reference in their respective entireties:

-   -   U.S. Design patent application Ser. No. 29/696,066, entitled        SURGICAL STAPLE CARTRIDGE RETAINER WITH FIRING SYSTEM        AUTHENTICATION KEY;    -   U.S. Design patent application Ser. No. 29/696,067, entitled        SURGICAL STAPLE CARTRIDGE RETAINER WITH CLOSURE SYSTEM        AUTHENTICATION KEY; and    -   U.S. Design patent application Ser. No. 29/696,072, entitled        SURGICAL STAPLE CARTRIDGE.

Applicant of the present application owns the following U.S. PatentApplications that were filed on Feb. 21, 2019 which are each hereinincorporated by reference in their respective entireties:

-   -   U.S. patent application Ser. No. 16/281,658, entitled METHODS        FOR CONTROLLING A POWERED SURGICAL STAPLER THAT HAS SEPARATE        ROTARY CLOSURE AND FIRING SYSTEMS;    -   U.S. patent application Ser. No. 16/281,670, entitled STAPLE        CARTRIDGE COMPRISING A LOCKOUT KEY CONFIGURED TO LIFT A FIRING        MEMBER;    -   U.S. patent application Ser. No. 16/281,675, entitled SURGICAL        STAPLERS WITH ARRANGEMENTS FOR MAINTAINING A FIRING MEMBER        THEREOF IN A LOCKED CONFIGURATION UNLESS A COMPATIBLE CARTRIDGE        HAS BEEN INSTALLED THEREIN;    -   U.S. patent application Ser. No. 16/281,685, entitled SURGICAL        INSTRUMENT COMPRISING CO-OPERATING LOCKOUT FEATURES;    -   U.S. patent application Ser. No. 16/281,693, entitled SURGICAL        STAPLING ASSEMBLY COMPRISING A LOCKOUT AND AN EXTERIOR ACCESS        ORIFICE TO PERMIT ARTIFICIAL UNLOCKING OF THE LOCKOUT;    -   U.S. patent application Ser. No. 16/281,704, entitled SURGICAL        STAPLING DEVICES WITH FEATURES FOR BLOCKING ADVANCEMENT OF A        CAMMING ASSEMBLY OF AN INCOMPATIBLE CARTRIDGE INSTALLED THEREIN;    -   U.S. patent application Ser. No. 16/281,707, entitled SURGICAL        INSTRUMENT COMPRISING A DEACTIVATABLE LOCKOUT;    -   U.S. patent application Ser. No. 16/281,741, entitled SURGICAL        INSTRUMENT COMPRISING A JAW CLOSURE LOCKOUT;    -   U.S. patent application Ser. No. 16/281,762, entitled SURGICAL        STAPLING DEVICES WITH CARTRIDGE COMPATIBLE CLOSURE AND FIRING        LOCKOUT ARRANGEMENTS;    -   U.S. patent application Ser. No. 16/281,660, entitled SURGICAL        STAPLE CARTRIDGE WITH FIRING MEMBER DRIVEN CAMMING ASSEMBLY THAT        HAS AN ONBOARD TISSUE CUTTING FEATURE;    -   U.S. patent application Ser. No. 16/281,666, entitled SURGICAL        STAPLING DEVICES WITH IMPROVED ROTARY DRIVEN CLOSURE SYSTEMS;    -   U.S. patent application Ser. No. 16/281,672, entitled SURGICAL        STAPLING DEVICES WITH ASYMMETRIC CLOSURE FEATURES;    -   U.S. patent application Ser. No. 16/281,678, entitled ROTARY        DRIVEN FIRING MEMBERS WITH DIFFERENT ANVIL AND FRAME ENGAGEMENT        FEATURES; and    -   U.S. patent application Ser. No. 16/281,682, entitled SURGICAL        STAPLING DEVICE WITH SEPARATE ROTARY DRIVEN CLOSURE AND FIRING        SYSTEMS AND FIRING MEMBER THAT ENGAGES BOTH JAWS WHILE FIRING.

Applicant of the present application owns the following U.S. ProvisionalPatent Applications, filed on Mar. 28, 2018, each of which is hereinincorporated by reference in its entirety:

-   -   U.S. Provisional Patent Application Ser. No. 62/649,302,        entitled INTERACTIVE SURGICAL SYSTEMS WITH ENCRYPTED        COMMUNICATION CAPABILITIES;    -   U.S. Provisional Patent Application Ser. No. 62/649,294,        entitled DATA STRIPPING METHOD TO INTERROGATE PATIENT RECORDS        AND CREATE ANONYMIZED RECORD;    -   U.S. Provisional Patent Application Ser. No. 62/649,300,        entitled SURGICAL HUB SITUATIONAL AWARENESS;    -   U.S. Provisional Patent Application Ser. No. 62/649,309,        entitled SURGICAL HUB SPATIAL AWARENESS TO DETERMINE DEVICES IN        OPERATING THEATER;    -   U.S. Provisional Patent Application Ser. No. 62/649,310,        entitled COMPUTER IMPLEMENTED INTERACTIVE SURGICAL SYSTEMS;    -   U.S. Provisional Patent Application Ser. No. 62/649,291,        entitled USE OF LASER LIGHT AND RED-GREEN-BLUE COLORATION TO        DETERMINE PROPERTIES OF BACK SCATTERED LIGHT;    -   U.S. Provisional Patent Application Ser. No. 62/649,296,        entitled ADAPTIVE CONTROL PROGRAM UPDATES FOR SURGICAL DEVICES;    -   U.S. Provisional Patent Application Ser. No. 62/649,333,        entitled CLOUD-BASED MEDICAL ANALYTICS FOR CUSTOMIZATION AND        RECOMMENDATIONS TO A USER;    -   U.S. Provisional Patent Application Ser. No. 62/649,327,        entitled CLOUD-BASED MEDICAL ANALYTICS FOR SECURITY AND        AUTHENTICATION TRENDS AND REACTIVE MEASURES;    -   U.S. Provisional Patent Application Ser. No. 62/649,315,        entitled DATA HANDLING AND PRIORITIZATION IN A CLOUD ANALYTICS        NETWORK;    -   U.S. Provisional Patent Application Ser. No. 62/649,313,        entitled CLOUD INTERFACE FOR COUPLED SURGICAL DEVICES;    -   U.S. Provisional Patent Application Ser. No. 62/649,320,        entitled DRIVE ARRANGEMENTS FOR ROBOT-ASSISTED SURGICAL        PLATFORMS;    -   U.S. Provisional Patent Application Ser. No. 62/649,307,        entitled AUTOMATIC TOOL ADJUSTMENTS FOR ROBOT-ASSISTED SURGICAL        PLATFORMS; and    -   U.S. Provisional Patent Application Ser. No. 62/649,323,        entitled SENSING ARRANGEMENTS FOR ROBOT-ASSISTED SURGICAL        PLATFORMS.

Applicant of the present application owns the following U.S. ProvisionalPatent Application, filed on Mar. 30, 2018, which is herein incorporatedby reference in its entirety:

-   -   U.S. Provisional Patent Application Ser. No. 62/650,887,        entitled SURGICAL SYSTEMS WITH OPTIMIZED SENSING CAPABILITIES.

Applicant of the present application owns the following U.S. PatentApplication, filed on Dec. 4, 2018, which is herein incorporated byreference in its entirety:

-   -   U.S. patent application Ser. No. 16/209,423, entitled METHOD OF        COMPRESSING TISSUE WITHIN A STAPLING DEVICE AND SIMULTANEOUSLY        DISPLAYING THE LOCATION OF THE TISSUE WITHIN THE JAWS.

Applicant of the present application owns the following U.S. PatentApplications that were filed on Aug. 20, 2018 and which are each hereinincorporated by reference in their respective entireties:

-   -   U.S. patent application Ser. No. 16/105,101, entitled METHOD FOR        FABRICATING SURGICAL STAPLER ANVILS;    -   U.S. patent application Ser. No. 16/105,183, entitled REINFORCED        DEFORMABLE ANVIL TIP FOR SURGICAL STAPLER ANVIL;    -   U.S. patent application Ser. No. 16/105,150, entitled SURGICAL        STAPLER ANVILS WITH STAPLE DIRECTING PROTRUSIONS AND TISSUE        STABILITY FEATURES;    -   U.S. patent application Ser. No. 16/105,098, entitled        FABRICATING TECHNIQUES FOR SURGICAL STAPLER ANVILS;    -   U.S. patent application Ser. No. 16/105,140, entitled SURGICAL        STAPLER ANVILS WITH TISSUE STOP FEATURES CONFIGURED TO AVOID        TISSUE PINCH;    -   U.S. patent application Ser. No. 16/105,081, entitled METHOD FOR        OPERATING A POWERED ARTICULATABLE SURGICAL INSTRUMENT;    -   U.S. patent application Ser. No. 16/105,094, entitled SURGICAL        INSTRUMENTS WITH PROGRESSIVE JAW CLOSURE ARRANGEMENTS;    -   U.S. patent application Ser. No. 16/105,097, entitled POWERED        SURGICAL INSTRUMENTS WITH CLUTCHING ARRANGEMENTS TO CONVERT        LINEAR DRIVE MOTIONS TO ROTARY DRIVE MOTIONS;    -   U.S. patent application Ser. No. 16/105,104, entitled POWERED        ARTICULATABLE SURGICAL INSTRUMENTS WITH CLUTCHING AND LOCKING        ARRANGEMENTS FOR LINKING AN ARTICULATION DRIVE SYSTEM TO A        FIRING DRIVE SYSTEM;    -   U.S. patent application Ser. No. 16/105,119, entitled        ARTICULATABLE MOTOR POWERED SURGICAL INSTRUMENTS WITH DEDICATED        ARTICULATION MOTOR ARRANGEMENTS;    -   U.S. patent application Ser. No. 16/105,160, entitled SWITCHING        ARRANGEMENTS FOR MOTOR POWERED ARTICULATABLE SURGICAL        INSTRUMENTS; and    -   U.S. Design patent application Ser. No. 29/660,252, entitled        SURGICAL STAPLER ANVILS.

Applicant of the present application owns the following U.S. PatentApplications that were filed on Aug. 3, 2017 and which are each hereinincorporated by reference in their respective entireties:

-   -   U.S. patent application Ser. No. 15/668,324, entitled SURGICAL        SYSTEM SHAFT INTERCONNECTION;    -   U.S. patent application Ser. No. 15/668,301, entitled SURGICAL        SYSTEM BAILOUT; and    -   U.S. patent application Ser. No. 15/668,319, entitled SURGICAL        SYSTEM COMPRISING AN ARTICULATION BAILOUT.

Applicant of the present application owns the following U.S. PatentApplications that were filed on Jun. 28, 2017 and which are each hereinincorporated by reference in their respective entireties:

-   -   U.S. patent application Ser. No. 15/635,693, entitled SURGICAL        INSTRUMENT COMPRISING AN OFFSET ARTICULATION JOINT;    -   U.S. patent application Ser. No. 15/635,729, entitled SURGICAL        INSTRUMENT COMPRISING AN ARTICULATION SYSTEM RATIO;    -   U.S. patent application Ser. No. 15/635,785, entitled SURGICAL        INSTRUMENT COMPRISING AN ARTICULATION SYSTEM RATIO;    -   U.S. patent application Ser. No. 15/635,808, entitled SURGICAL        INSTRUMENT COMPRISING FIRING MEMBER SUPPORTS;    -   U.S. patent application Ser. No. 15/635,837, entitled SURGICAL        INSTRUMENT COMPRISING AN ARTICULATION SYSTEM LOCKABLE TO A        FRAME;    -   U.S. patent application Ser. No. 15/635,941, entitled SURGICAL        INSTRUMENT COMPRISING AN ARTICULATION SYSTEM LOCKABLE BY A        CLOSURE SYSTEM;    -   U.S. patent application Ser. No. 15/636,029, entitled SURGICAL        INSTRUMENT COMPRISING A SHAFT INCLUDING A HOUSING ARRANGEMENT;    -   U.S. patent application Ser. No. 15/635,958, entitled SURGICAL        INSTRUMENT COMPRISING SELECTIVELY ACTUATABLE ROTATABLE COUPLERS;    -   U.S. patent application Ser. No. 15/635,981, entitled SURGICAL        STAPLING INSTRUMENTS COMPRISING SHORTENED STAPLE CARTRIDGE        NOSES;    -   U.S. patent application Ser. No. 15/636,009, entitled SURGICAL        INSTRUMENT COMPRISING A SHAFT INCLUDING A CLOSURE TUBE PROFILE;    -   U.S. patent application Ser. No. 15/635,663, entitled METHOD FOR        ARTICULATING A SURGICAL INSTRUMENT;    -   U.S. patent application Ser. No. 15/635,530, entitled SURGICAL        INSTRUMENTS WITH ARTICULATABLE END EFFECTOR WITH AXIALLY        SHORTENED ARTICULATION JOINT CONFIGURATIONS;    -   U.S. patent application Ser. No. 15/635,549, entitled SURGICAL        INSTRUMENTS WITH OPEN AND CLOSABLE JAWS AND AXIALLY MOVABLE        FIRING MEMBER THAT IS INITIALLY PARKED IN CLOSE PROXIMITY TO THE        JAWS PRIOR TO FIRING;    -   U.S. patent application Ser. No. 15/635,559, entitled SURGICAL        INSTRUMENTS WITH JAWS CONSTRAINED TO PIVOT ABOUT AN AXIS UPON        CONTACT WITH A CLOSURE MEMBER THAT IS PARKED IN CLOSE PROXIMITY        TO THE PIVOT AXIS;    -   U.S. patent application Ser. No. 15/635,578, entitled SURGICAL        END EFFECTORS WITH IMPROVED JAW APERTURE ARRANGEMENTS;    -   U.S. patent application Ser. No. 15/635,594, entitled SURGICAL        CUTTING AND FASTENING DEVICES WITH PIVOTABLE ANVIL WITH A TISSUE        LOCATING ARRANGEMENT IN CLOSE PROXIMITY TO AN ANVIL PIVOT AXIS;    -   U.S. patent application Ser. No. 15/635,612, entitled JAW        RETAINER ARRANGEMENT FOR RETAINING A PIVOTABLE SURGICAL        INSTRUMENT JAW IN PIVOTABLE RETAINING ENGAGEMENT WITH A SECOND        SURGICAL INSTRUMENT JAW;    -   U.S. patent application Ser. No. 15/635,621, entitled SURGICAL        INSTRUMENT WITH POSITIVE JAW OPENING FEATURES;    -   U.S. patent application Ser. No. 15/635,631, entitled SURGICAL        INSTRUMENT WITH AXIALLY MOVABLE CLOSURE MEMBER;    -   U.S. patent application Ser. No. 15/635,521, entitled SURGICAL        INSTRUMENT LOCKOUT ARRANGEMENT;    -   U.S. Design patent application Ser. No. 29/609,083, entitled        SURGICAL INSTRUMENT SHAFT;    -   U.S. Design patent application Ser. No. 29/609,087, entitled        SURGICAL FORMING ANVIL;    -   U.S. Design patent application Ser. No. 29/609,093, entitled        SURGICAL FASTENER CARTRIDGE;    -   U.S. Design patent application Ser. No. 29/609,121, entitled        SURGICAL INSTRUMENT;    -   U.S. Design patent application Ser. No. 29/609,125, entitled        SURGICAL INSTRUMENT;    -   U.S. Design patent application Ser. No. 29/609,128, entitled        SURGICAL INSTRUMENT; and    -   U.S. Design patent application Ser. No. 29/609,129, entitled        DISPLAY SCREEN PORTION OF A SURGICAL INSTRUMENT HAVING A        GRAPHICAL USER INTERFACE.

Applicant of the present application owns the following U.S. PatentApplications that were filed on Jun. 27, 2017 and which are each hereinincorporated by reference in their respective entireties:

-   -   U.S. patent application Ser. No. 15/634,024, entitled SURGICAL        ANVIL MANUFACTURING METHODS;    -   U.S. patent application Ser. No. 15/634,035, entitled SURGICAL        ANVIL ARRANGEMENTS;    -   U.S. patent application Ser. No. 15/634,046, entitled SURGICAL        ANVIL ARRANGEMENTS;    -   U.S. patent application Ser. No. 15/634,054, entitled SURGICAL        ANVIL ARRANGEMENTS;    -   U.S. patent application Ser. No. 15/634,068, entitled SURGICAL        FIRING MEMBER ARRANGEMENTS;    -   U.S. patent application Ser. No. 15/634,076, entitled STAPLE        FORMING POCKET ARRANGEMENTS;    -   U.S. patent application Ser. No. 15/634,090, entitled STAPLE        FORMING POCKET ARRANGEMENTS;    -   U.S. patent application Ser. No. 15/634,099, entitled SURGICAL        END EFFECTORS AND ANVILS; and    -   U.S. patent application Ser. No. 15/634,117, entitled        ARTICULATION SYSTEMS FOR SURGICAL INSTRUMENTS.

Applicant of the present application owns the following U.S. PatentApplications that were filed on Dec. 21, 2016 and which are each hereinincorporated by reference in their respective entireties:

-   -   U.S. patent application Ser. No. 15/386,185, entitled SURGICAL        STAPLING INSTRUMENTS AND REPLACEABLE TOOL ASSEMBLIES THEREOF;    -   U.S. patent application Ser. No. 15/386,230, entitled        ARTICULATABLE SURGICAL STAPLING INSTRUMENTS;    -   U.S. patent application Ser. No. 15/386,221, entitled LOCKOUT        ARRANGEMENTS FOR SURGICAL END EFFECTORS;    -   U.S. patent application Ser. No. 15/386,209, entitled SURGICAL        END EFFECTORS AND FIRING MEMBERS THEREOF;    -   U.S. patent application Ser. No. 15/386,198, entitled LOCKOUT        ARRANGEMENTS FOR SURGICAL END EFFECTORS AND REPLACEABLE TOOL        ASSEMBLIES;    -   U.S. patent application Ser. No. 15/386,240, entitled SURGICAL        END EFFECTORS AND ADAPTABLE FIRING MEMBERS THEREFOR;    -   U.S. patent application Ser. No. 15/385,939, entitled STAPLE        CARTRIDGES AND ARRANGEMENTS OF STAPLES AND STAPLE CAVITIES        THEREIN;    -   U.S. patent application Ser. No. 15/385,941, entitled SURGICAL        TOOL ASSEMBLIES WITH CLUTCHING ARRANGEMENTS FOR SHIFTING BETWEEN        CLOSURE SYSTEMS WITH CLOSURE STROKE REDUCTION FEATURES AND        ARTICULATION AND FIRING SYSTEMS;    -   U.S. patent application Ser. No. 15/385,943, entitled SURGICAL        STAPLING INSTRUMENTS AND STAPLE-FORMING ANVILS;    -   U.S. patent application Ser. No. 15/385,950, entitled SURGICAL        TOOL ASSEMBLIES WITH CLOSURE STROKE REDUCTION FEATURES;    -   U.S. patent application Ser. No. 15/385,945, entitled STAPLE        CARTRIDGES AND ARRANGEMENTS OF STAPLES AND STAPLE CAVITIES        THEREIN;    -   U.S. patent application Ser. No. 15/385,946, entitled SURGICAL        STAPLING INSTRUMENTS AND STAPLE-FORMING ANVILS;    -   U.S. patent application Ser. No. 15/385,951, entitled SURGICAL        INSTRUMENTS WITH JAW OPENING FEATURES FOR INCREASING A JAW        OPENING DISTANCE;    -   U.S. patent application Ser. No. 15/385,953, entitled METHODS OF        STAPLING TISSUE;    -   U.S. patent application Ser. No. 15/385,954, entitled FIRING        MEMBERS WITH NON-PARALLEL JAW ENGAGEMENT FEATURES FOR SURGICAL        END EFFECTORS;    -   U.S. patent application Ser. No. 15/385,955, entitled SURGICAL        END EFFECTORS WITH EXPANDABLE TISSUE STOP ARRANGEMENTS;    -   U.S. patent application Ser. No. 15/385,948, entitled SURGICAL        STAPLING INSTRUMENTS AND STAPLE-FORMING ANVILS;    -   U.S. patent application Ser. No. 15/385,956, entitled SURGICAL        INSTRUMENTS WITH POSITIVE JAW OPENING FEATURES;    -   U.S. patent application Ser. No. 15/385,958, entitled SURGICAL        INSTRUMENTS WITH LOCKOUT ARRANGEMENTS FOR PREVENTING FIRING        SYSTEM ACTUATION UNLESS AN UNSPENT STAPLE CARTRIDGE IS PRESENT;    -   U.S. patent application Ser. No. 15/385,947, entitled STAPLE        CARTRIDGES AND ARRANGEMENTS OF STAPLES AND STAPLE CAVITIES        THEREIN;    -   U.S. patent application Ser. No. 15/385,896, entitled METHOD FOR        RESETTING A FUSE OF A SURGICAL INSTRUMENT SHAFT;    -   U.S. patent application Ser. No. 15/385,898, entitled STAPLE        FORMING POCKET ARRANGEMENT TO ACCOMMODATE DIFFERENT TYPES OF        STAPLES;    -   U.S. patent application Ser. No. 15/385,899, entitled SURGICAL        INSTRUMENT COMPRISING IMPROVED JAW CONTROL;    -   U.S. patent application Ser. No. 15/385,901, entitled STAPLE        CARTRIDGE AND STAPLE CARTRIDGE CHANNEL COMPRISING WINDOWS        DEFINED THEREIN;    -   U.S. patent application Ser. No. 15/385,902, entitled SURGICAL        INSTRUMENT COMPRISING A CUTTING MEMBER;    -   U.S. patent application Ser. No. 15/385,904, entitled STAPLE        FIRING MEMBER COMPRISING A MISSING CARTRIDGE AND/OR SPENT        CARTRIDGE LOCKOUT;    -   U.S. patent application Ser. No. 15/385,905, entitled FIRING        ASSEMBLY COMPRISING A LOCKOUT;    -   U.S. patent application Ser. No. 15/385,907, entitled SURGICAL        INSTRUMENT SYSTEM COMPRISING AN END EFFECTOR LOCKOUT AND A        FIRING ASSEMBLY LOCKOUT;    -   U.S. patent application Ser. No. 15/385,908, entitled FIRING        ASSEMBLY COMPRISING A FUSE;    -   U.S. patent application Ser. No. 15/385,909, entitled FIRING        ASSEMBLY COMPRISING A MULTIPLE FAILED-STATE FUSE;    -   U.S. patent application Ser. No. 15/385,920, entitled STAPLE        FORMING POCKET ARRANGEMENTS;    -   U.S. patent application Ser. No. 15/385,913, entitled ANVIL        ARRANGEMENTS FOR SURGICAL STAPLE/FASTENERS;    -   U.S. patent application Ser. No. 15/385,914, entitled METHOD OF        DEFORMING STAPLES FROM TWO DIFFERENT TYPES OF STAPLE CARTRIDGES        WITH THE SAME SURGICAL STAPLING INSTRUMENT;    -   U.S. patent application Ser. No. 15/385,893, entitled        BILATERALLY ASYMMETRIC STAPLE FORMING POCKET PAIRS;    -   U.S. patent application Ser. No. 15/385,929, entitled CLOSURE        MEMBERS WITH CAM SURFACE ARRANGEMENTS FOR SURGICAL INSTRUMENTS        WITH SEPARATE AND DISTINCT CLOSURE AND FIRING SYSTEMS;    -   U.S. patent application Ser. No. 15/385, 911, entitled SURGICAL        STAPLE/FASTENERS WITH INDEPENDENTLY ACTUATABLE CLOSING AND        FIRING SYSTEMS;    -   U.S. patent application Ser. No. 15/385,927, entitled SURGICAL        STAPLING INSTRUMENTS WITH SMART STAPLE CARTRIDGES;    -   U.S. patent application Ser. No. 15/385,917, entitled STAPLE        CARTRIDGE COMPRISING STAPLES WITH DIFFERENT CLAMPING BREADTHS;    -   U.S. patent application Ser. No. 15/385,900, entitled STAPLE        FORMING POCKET ARRANGEMENTS COMPRISING PRIMARY SIDEWALLS AND        POCKET SIDEWALLS;    -   U.S. patent application Ser. No. 15/385,931, entitled        NO-CARTRIDGE AND SPENT CARTRIDGE LOCKOUT ARRANGEMENTS FOR        SURGICAL STAPLE/FASTENERS;    -   U.S. patent application Ser. No. 15/385,915, entitled FIRING        MEMBER PIN ANGLE;    -   U.S. patent application Ser. No. 15/385,897, entitled STAPLE        FORMING POCKET ARRANGEMENTS COMPRISING ZONED FORMING SURFACE        GROOVES;    -   U.S. patent application Ser. No. 15/385,922, entitled SURGICAL        INSTRUMENT WITH MULTIPLE FAILURE RESPONSE MODES;    -   U.S. patent application Ser. No. 15/385,924, entitled SURGICAL        INSTRUMENT WITH PRIMARY AND SAFETY PROCESSORS;    -   U.S. patent application Ser. No. 15/385,912, entitled SURGICAL        INSTRUMENTS WITH JAWS THAT ARE PIVOTABLE ABOUT A FIXED AXIS AND        INCLUDE SEPARATE AND DISTINCT CLOSURE AND FIRING SYSTEMS;    -   U.S. patent application Ser. No. 15/385,910, entitled ANVIL        HAVING A KNIFE SLOT WIDTH;    -   U.S. patent application Ser. No. 15/385,906, entitled FIRING        MEMBER PIN CONFIGURATIONS;    -   U.S. patent application Ser. No. 15/386,188, entitled STEPPED        STAPLE CARTRIDGE WITH ASYMMETRICAL STAPLES;    -   U.S. patent application Ser. No. 15/386,192, entitled STEPPED        STAPLE CARTRIDGE WITH TISSUE RETENTION AND GAP SETTING FEATURES;    -   U.S. patent application Ser. No. 15/386,206, entitled STAPLE        CARTRIDGE WITH DEFORMABLE DRIVER RETENTION FEATURES;    -   U.S. patent application Ser. No. 15/386,226, entitled DURABILITY        FEATURES FOR END EFFECTORS AND FIRING ASSEMBLIES OF SURGICAL        STAPLING INSTRUMENTS;    -   U.S. patent application Ser. No. 15/386,222, entitled SURGICAL        STAPLING INSTRUMENTS HAVING END EFFECTORS WITH POSITIVE OPENING        FEATURES;    -   U.S. patent application Ser. No. 15/386,236, entitled CONNECTION        PORTIONS FOR DEPOSABLE LOADING UNITS FOR SURGICAL STAPLING        INSTRUMENTS;    -   U.S. patent application Ser. No. 15/385,887, entitled METHOD FOR        ATTACHING A SHAFT ASSEMBLY TO A SURGICAL INSTRUMENT AND,        ALTERNATIVELY, TO A SURGICAL ROBOT;    -   U.S. patent application Ser. No. 15/385,889, entitled SHAFT        ASSEMBLY COMPRISING A MANUALLY-OPERABLE RETRACTION SYSTEM FOR        USE WITH A MOTORIZED SURGICAL INSTRUMENT SYSTEM;    -   U.S. patent application Ser. No. 15/385,890, entitled SHAFT        ASSEMBLY COMPRISING SEPARATELY ACTUATABLE AND RETRACTABLE        SYSTEMS;    -   U.S. patent application Ser. No. 15/385,891, entitled SHAFT        ASSEMBLY COMPRISING A CLUTCH CONFIGURED TO ADAPT THE OUTPUT OF A        ROTARY FIRING MEMBER TO TWO DIFFERENT SYSTEMS;    -   U.S. patent application Ser. No. 15/385,892, entitled SURGICAL        SYSTEM COMPRISING A FIRING MEMBER ROTATABLE INTO AN ARTICULATION        STATE TO ARTICULATE AN END EFFECTOR OF THE SURGICAL SYSTEM;    -   U.S. patent application Ser. No. 15/385,894, entitled SHAFT        ASSEMBLY COMPRISING A LOCKOUT;    -   U.S. patent application Ser. No. 15/385,895, entitled SHAFT        ASSEMBLY COMPRISING FIRST AND SECOND ARTICULATION LOCKOUTS;    -   U.S. patent application Ser. No. 15/385,916, entitled SURGICAL        STAPLING SYSTEMS;    -   U.S. patent application Ser. No. 15/385,918, entitled SURGICAL        STAPLING SYSTEMS;    -   U.S. patent application Ser. No. 15/385,919, entitled SURGICAL        STAPLING SYSTEMS;    -   U.S. patent application Ser. No. 15/385,921, entitled SURGICAL        STAPLE/FASTENER CARTRIDGE WITH MOVABLE CAMMING MEMBER CONFIGURED        TO DISENGAGE FIRING MEMBER LOCKOUT FEATURES;    -   U.S. patent application Ser. No. 15/385,923, entitled SURGICAL        STAPLING SYSTEMS;    -   U.S. patent application Ser. No. 15/385,925, entitled JAW        ACTUATED LOCK ARRANGEMENTS FOR PREVENTING ADVANCEMENT OF A        FIRING MEMBER IN A SURGICAL END EFFECTOR UNLESS AN UNFIRED        CARTRIDGE IS INSTALLED IN THE END EFFECTOR;    -   U.S. patent application Ser. No. 15/385,926, entitled AXIALLY        MOVABLE CLOSURE SYSTEM ARRANGEMENTS FOR APPLYING CLOSURE MOTIONS        TO JAWS OF SURGICAL INSTRUMENTS;    -   U.S. patent application Ser. No. 15/385,928, entitled PROTECTIVE        COVER ARRANGEMENTS FOR A JOINT INTERFACE BETWEEN A MOVABLE JAW        AND ACTUATOR SHAFT OF A SURGICAL INSTRUMENT;    -   U.S. patent application Ser. No. 15/385,930, entitled SURGICAL        END EFFECTOR WITH TWO SEPARATE COOPERATING OPENING FEATURES FOR        OPENING AND CLOSING END EFFECTOR JAWS;    -   U.S. patent application Ser. No. 15/385,932, entitled        ARTICULATABLE SURGICAL END EFFECTOR WITH ASYMMETRIC SHAFT        ARRANGEMENT;    -   U.S. patent application Ser. No. 15/385,933, entitled        ARTICULATABLE SURGICAL INSTRUMENT WITH INDEPENDENT PIVOTABLE        LINKAGE DISTAL OF AN ARTICULATION LOCK;    -   U.S. patent application Ser. No. 15/385,934, entitled        ARTICULATION LOCK ARRANGEMENTS FOR LOCKING AN END EFFECTOR IN AN        ARTICULATED POSITION IN RESPONSE TO ACTUATION OF A JAW CLOSURE        SYSTEM;    -   U.S. patent application Ser. No. 15/385,935, entitled LATERALLY        ACTUATABLE ARTICULATION LOCK ARRANGEMENTS FOR LOCKING AN END        EFFECTOR OF A SURGICAL INSTRUMENT IN AN ARTICULATED        CONFIGURATION; and    -   U.S. patent application Ser. No. 15/385,936, entitled        ARTICULATABLE SURGICAL INSTRUMENTS WITH ARTICULATION STROKE        AMPLIFICATION FEATURES.

Applicant of the present application owns the following U.S. PatentApplications that were filed on Jun. 24, 2016 and which are each hereinincorporated by reference in their respective entireties:

-   -   U.S. patent application Ser. No. 15/191,775, entitled STAPLE        CARTRIDGE COMPRISING WIRE STAPLES AND STAMPED STAPLES;    -   U.S. patent application Ser. No. 15/191,807, entitled STAPLING        SYSTEM FOR USE WITH WIRE STAPLES AND STAMPED STAPLES;    -   U.S. patent application Ser. No. 15/191,834, entitled STAMPED        STAPLES AND STAPLE CARTRIDGES USING THE SAME;    -   U.S. patent application Ser. No. 15/191,788, entitled STAPLE        CARTRIDGE COMPRISING OVERDRIVEN STAPLES; and    -   U.S. patent application Ser. No. 15/191,818, entitled STAPLE        CARTRIDGE COMPRISING OFFSET LONGITUDINAL STAPLE ROWS.

Applicant of the present application owns the following U.S. PatentApplications that were filed on Jun. 24, 2016 and which are each hereinincorporated by reference in their respective entireties:

-   -   U.S. Design patent application Ser. No. 29/569,218, entitled        SURGICAL FASTENER;    -   U.S. Design patent application Ser. No. 29/569,227, entitled        SURGICAL FASTENER;    -   U.S. Design patent application Ser. No. 29/569,259, entitled        SURGICAL FASTENER CARTRIDGE; and    -   U.S. Design patent application Ser. No. 29/569,264, entitled        SURGICAL FASTENER CARTRIDGE.

Applicant of the present application owns the following patentapplications that were filed on Apr. 1, 2016 and which are each hereinincorporated by reference in their respective entirety:

-   -   U.S. patent application Ser. No. 15/089,325, entitled METHOD FOR        OPERATING A SURGICAL STAPLING SYSTEM;    -   U.S. patent application Ser. No. 15/089,321, entitled MODULAR        SURGICAL STAPLING SYSTEM COMPRISING A DISPLAY;    -   U.S. patent application Ser. No. 15/089,326, entitled SURGICAL        STAPLING SYSTEM COMPRISING A DISPLAY INCLUDING A RE-ORIENTABLE        DISPLAY FIELD;    -   U.S. patent application Ser. No. 15/089,263, entitled SURGICAL        INSTRUMENT HANDLE ASSEMBLY WITH RECONFIGURABLE GRIP PORTION;    -   U.S. patent application Ser. No. 15/089,262, entitled ROTARY        POWERED SURGICAL INSTRUMENT WITH MANUALLY ACTUATABLE BAILOUT        SYSTEM;    -   U.S. patent application Ser. No. 15/089,277, entitled SURGICAL        CUTTING AND STAPLING END EFFECTOR WITH ANVIL CONCENTRIC DRIVE        MEMBER;    -   U.S. patent application Ser. No. 15/089,296, entitled        INTERCHANGEABLE SURGICAL TOOL ASSEMBLY WITH A SURGICAL END        EFFECTOR THAT IS SELECTIVELY ROTATABLE ABOUT A SHAFT AXIS;    -   U.S. patent application Ser. No. 15/089,258, entitled SURGICAL        STAPLING SYSTEM COMPRISING A SHIFTABLE TRANSMISSION;    -   U.S. patent application Ser. No. 15/089,278, entitled SURGICAL        STAPLING SYSTEM CONFIGURED TO PROVIDE SELECTIVE CUTTING OF        TISSUE;    -   U.S. patent application Ser. No. 15/089,284, entitled SURGICAL        STAPLING SYSTEM COMPRISING A CONTOURABLE SHAFT;    -   U.S. patent application Ser. No. 15/089,295, entitled SURGICAL        STAPLING SYSTEM COMPRISING A TISSUE COMPRESSION LOCKOUT;    -   U.S. patent application Ser. No. 15/089,300, entitled SURGICAL        STAPLING SYSTEM COMPRISING AN UNCLAMPING LOCKOUT;    -   U.S. patent application Ser. No. 15/089,196, entitled SURGICAL        STAPLING SYSTEM COMPRISING A JAW CLOSURE LOCKOUT;    -   U.S. patent application Ser. No. 15/089,203, entitled SURGICAL        STAPLING SYSTEM COMPRISING A JAW ATTACHMENT LOCKOUT;    -   U.S. patent application Ser. No. 15/089,210, entitled SURGICAL        STAPLING SYSTEM COMPRISING A SPENT CARTRIDGE LOCKOUT;    -   U.S. patent application Ser. No. 15/089,324, entitled SURGICAL        INSTRUMENT COMPRISING A SHIFTING MECHANISM;    -   U.S. patent application Ser. No. 15/089,335, entitled SURGICAL        STAPLING INSTRUMENT COMPRISING MULTIPLE LOCKOUTS;    -   U.S. patent application Ser. No. 15/089,339, entitled SURGICAL        STAPLING INSTRUMENT;    -   U.S. patent application Ser. No. 15/089,253, entitled SURGICAL        STAPLING SYSTEM CONFIGURED TO APPLY ANNULAR ROWS OF STAPLES        HAVING DIFFERENT HEIGHTS;    -   U.S. patent application Ser. No. 15/089,304, entitled SURGICAL        STAPLING SYSTEM COMPRISING A GROOVED FORMING POCKET;    -   U.S. patent application Ser. No. 15/089,331, entitled ANVIL        MODIFICATION MEMBERS FOR SURGICAL STAPLE/FASTENERS;    -   U.S. patent application Ser. No. 15/089,336, entitled STAPLE        CARTRIDGES WITH ATRAUMATIC FEATURES;    -   U.S. patent application Ser. No. 15/089,312, entitled CIRCULAR        STAPLING SYSTEM COMPRISING AN INCISABLE TISSUE SUPPORT;    -   U.S. patent application Ser. No. 15/089,309, entitled CIRCULAR        STAPLING SYSTEM COMPRISING ROTARY FIRING SYSTEM; and    -   U.S. patent application Ser. No. 15/089,349, entitled CIRCULAR        STAPLING SYSTEM COMPRISING LOAD CONTROL.

Applicant of the present application also owns the U.S. PatentApplications identified below which were filed on Dec. 31, 2015 whichare each herein incorporated by reference in their respective entirety:

-   -   U.S. patent application Ser. No. 14/984,488, entitled MECHANISMS        FOR COMPENSATING FOR BATTERY PACK FAILURE IN POWERED SURGICAL        INSTRUMENTS;    -   U.S. patent application Ser. No. 14/984,525, entitled MECHANISMS        FOR COMPENSATING FOR DRIVETRAIN FAILURE IN POWERED SURGICAL        INSTRUMENTS; and    -   U.S. patent application Ser. No. 14/984,552, entitled SURGICAL        INSTRUMENTS WITH SEPARABLE MOTORS AND MOTOR CONTROL CIRCUITS.

Applicant of the present application also owns the U.S. PatentApplications identified below which were filed on Feb. 9, 2016 which areeach herein incorporated by reference in their respective entirety:

-   -   U.S. patent application Ser. No. 15/019,220, entitled SURGICAL        INSTRUMENT WITH ARTICULATING AND AXIALLY TRANSLATABLE END        EFFECTOR;    -   U.S. patent application Ser. No. 15/019,228, entitled SURGICAL        INSTRUMENTS WITH MULTIPLE LINK ARTICULATION ARRANGEMENTS;    -   U.S. patent application Ser. No. 15/019,196, entitled SURGICAL        INSTRUMENT ARTICULATION MECHANISM WITH SLOTTED SECONDARY        CONSTRAINT;    -   U.S. patent application Ser. No. 15/019,206, entitled SURGICAL        INSTRUMENTS WITH AN END EFFECTOR THAT IS HIGHLY ARTICULATABLE        RELATIVE TO AN ELONGATE SHAFT ASSEMBLY;    -   U.S. patent application Ser. No. 15/019,215, entitled SURGICAL        INSTRUMENTS WITH NON-SYMMETRICAL ARTICULATION ARRANGEMENTS;    -   U.S. patent application Ser. No. 15/019,227, entitled        ARTICULATABLE SURGICAL INSTRUMENTS WITH SINGLE ARTICULATION LINK        ARRANGEMENTS;    -   U.S. patent application Ser. No. 15/019,235, entitled SURGICAL        INSTRUMENTS WITH TENSIONING ARRANGEMENTS FOR CABLE DRIVEN        ARTICULATION SYSTEMS;    -   U.S. patent application Ser. No. 15/019,230, entitled        ARTICULATABLE SURGICAL INSTRUMENTS WITH OFF-AXIS FIRING BEAM        ARRANGEMENTS; and    -   U.S. patent application Ser. No. 15/019,245, entitled SURGICAL        INSTRUMENTS WITH CLOSURE STROKE REDUCTION ARRANGEMENTS.

Applicant of the present application also owns the U.S. PatentApplications identified below which were filed on Feb. 12, 2016 whichare each herein incorporated by reference in their respective entirety:

-   -   U.S. patent application Ser. No. 15/043,254, entitled MECHANISMS        FOR COMPENSATING FOR DRIVETRAIN FAILURE IN POWERED SURGICAL        INSTRUMENTS;    -   U.S. patent application Ser. No. 15/043,259, entitled MECHANISMS        FOR COMPENSATING FOR DRIVETRAIN FAILURE IN POWERED SURGICAL        INSTRUMENTS;    -   U.S. patent application Ser. No. 15/043,275, entitled MECHANISMS        FOR COMPENSATING FOR DRIVETRAIN FAILURE IN POWERED SURGICAL        INSTRUMENTS; and    -   U.S. patent application Ser. No. 15/043,289, entitled MECHANISMS        FOR COMPENSATING FOR DRIVETRAIN FAILURE IN POWERED SURGICAL        INSTRUMENTS.

Applicant of the present application owns the following patentapplications that were filed on Jun. 18, 2015 and which are each hereinincorporated by reference in their respective entirety:

-   -   U.S. patent application Ser. No. 14/742,925, entitled SURGICAL        END EFFECTORS WITH POSITIVE JAW OPENING ARRANGEMENTS, now U.S.        Pat. No. 10,182,818;    -   U.S. patent application Ser. No. 14/742,941, entitled SURGICAL        END EFFECTORS WITH DUAL CAM ACTUATED JAW CLOSING FEATURES, now        U.S. Pat. No. 10,052,102;    -   U.S. patent application Ser. No. 14/742,914, entitled MOVABLE        FIRING BEAM SUPPORT ARRANGEMENTS FOR ARTICULATABLE SURGICAL        INSTRUMENTS, now U.S. Pat. No. 10,405,863;    -   U.S. patent application Ser. No. 14/742,900, entitled        ARTICULATABLE SURGICAL INSTRUMENTS WITH COMPOSITE FIRING BEAM        STRUCTURES WITH CENTER FIRING SUPPORT MEMBER FOR ARTICULATION        SUPPORT, now U.S. Pat. No. 10,335,149;    -   U.S. patent application Ser. No. 14/742,885, entitled DUAL        ARTICULATION DRIVE SYSTEM ARRANGEMENTS FOR ARTICULATABLE        SURGICAL INSTRUMENTS, now U.S. Pat. No. 10,368,861; and    -   U.S. patent application Ser. No. 14/742,876, entitled PUSH/PULL        ARTICULATION DRIVE SYSTEMS FOR ARTICULATABLE SURGICAL        INSTRUMENTS, now U.S. Pat. No. 10,178,992.

Applicant of the present application owns the following patentapplications that were filed on Mar. 6, 2015 and which are each hereinincorporated by reference in their respective entirety:

-   -   U.S. patent application Ser. No. 14/640,746, entitled POWERED        SURGICAL INSTRUMENT, now U.S. Pat. No. 9,808,246;    -   U.S. patent application Ser. No. 14/640,795, entitled MULTIPLE        LEVEL THRESHOLDS TO MODIFY OPERATION OF POWERED SURGICAL        INSTRUMENTS, now U.S. Pat. No. 10,441,279;    -   U.S. patent application Ser. No. 14/640,832, entitled ADAPTIVE        TISSUE COMPRESSION TECHNIQUES TO ADJUST CLOSURE RATES FOR        MULTIPLE TISSUE TYPES, now U.S. Patent Application Publication        No. 2016/0256154;    -   U.S. patent application Ser. No. 14/640,935, entitled OVERLAID        MULTI SENSOR RADIO FREQUENCY (RF) ELECTRODE SYSTEM TO MEASURE        TISSUE COMPRESSION, now U.S. Patent Application Publication No.        2016/0256071;    -   U.S. patent application Ser. No. 14/640,831, entitled MONITORING        SPEED CONTROL AND PRECISION INCREMENTING OF MOTOR FOR POWERED        SURGICAL INSTRUMENTS, now U.S. Pat. No. 9,985,148;    -   U.S. patent application Ser. No. 14/640,859, entitled TIME        DEPENDENT EVALUATION OF SENSOR DATA TO DETERMINE STABILITY,        CREEP, AND VISCOELASTIC ELEMENTS OF MEASURES, now U.S. Pat. No.        10,052,044;    -   U.S. patent application Ser. No. 14/640,817, entitled        INTERACTIVE FEEDBACK SYSTEM FOR POWERED SURGICAL INSTRUMENTS,        now U.S. Pat. No. 9,924,961;    -   U.S. patent application Ser. No. 14/640,844, entitled CONTROL        TECHNIQUES AND SUB-PROCESSOR CONTAINED WITHIN MODULAR SHAFT WITH        SELECT CONTROL PROCESSING FROM HANDLE, now U.S. Pat. No.        10,045,776;    -   U.S. patent application Ser. No. 14/640,837, entitled SMART        SENSORS WITH LOCAL SIGNAL PROCESSING, now U.S. Pat. No.        9,993,248;    -   U.S. patent application Ser. No. 14/640,765, entitled SYSTEM FOR        DETECTING THE MIS-INSERTION OF A STAPLE CARTRIDGE INTO A        SURGICAL STAPLE/FASTENER, now U.S. Patent Application        Publication No. 2016/0256160;    -   U.S. patent application Ser. No. 14/640,799, entitled SIGNAL AND        POWER COMMUNICATION SYSTEM POSITIONED ON A ROTATABLE SHAFT, now        U.S. Pat. No. 9,901,342; and    -   U.S. patent application Ser. No. 14/640,780, entitled SURGICAL        INSTRUMENT COMPRISING A LOCKABLE BATTERY HOUSING, now U.S. Pat.        No. 10,245,033.

Applicant of the present application owns the following patentapplications that were filed on Feb. 27, 2015, and which are each hereinincorporated by reference in their respective entirety:

-   -   U.S. patent application Ser. No. 14/633,576, entitled SURGICAL        INSTRUMENT SYSTEM COMPRISING AN INSPECTION STATION, now U.S.        Pat. No. 10,045,779;    -   U.S. patent application Ser. No. 14/633,546, entitled SURGICAL        APPARATUS CONFIGURED TO ASSESS WHETHER A PERFORMANCE PARAMETER        OF THE SURGICAL APPARATUS IS WITHIN AN ACCEPTABLE PERFORMANCE        BAND, now U.S. Pat. No. 10,180,463;    -   U.S. patent application Ser. No. 14/633,560, entitled SURGICAL        CHARGING SYSTEM THAT CHARGES AND/OR CONDITIONS ONE OR MORE        BATTERIES, now U.S. Patent Application Publication No.        2016/0249910;    -   U.S. patent application Ser. No. 14/633,566, entitled CHARGING        SYSTEM THAT ENABLES EMERGENCY RESOLUTIONS FOR CHARGING A        BATTERY, now U.S. Pat. No. 10,182,816;    -   U.S. patent application Ser. No. 14/633,555, entitled SYSTEM FOR        MONITORING WHETHER A SURGICAL INSTRUMENT NEEDS TO BE SERVICED,        now U.S. Pat. No. 10,321,907;    -   U.S. patent application Ser. No. 14/633,542, entitled REINFORCED        BATTERY FOR A SURGICAL INSTRUMENT, now U.S. Pat. No. 9,931,118;    -   U.S. patent application Ser. No. 14/633,548, entitled POWER        ADAPTER FOR A SURGICAL INSTRUMENT, now U.S. Pat. No. 10,245,028;    -   U.S. patent application Ser. No. 14/633,526, entitled ADAPTABLE        SURGICAL INSTRUMENT HANDLE, now U.S. Pat. No. 9,993,258;    -   U.S. patent application Ser. No. 14/633,541, entitled MODULAR        STAPLING ASSEMBLY, now U.S. Pat. No. 10,226,250; and    -   U.S. patent application Ser. No. 14/633,562, entitled SURGICAL        APPARATUS CONFIGURED TO TRACK AN END-OF-LIFE PARAMETER, now U.S.        Pat. No. 10,159,483.

Applicant of the present application owns the following patentapplications that were filed on Dec. 18, 2014 and which are each hereinincorporated by reference in their respective entirety:

-   -   U.S. patent application Ser. No. 14/574,478, entitled SURGICAL        INSTRUMENT SYSTEMS COMPRISING AN ARTICULATABLE END EFFECTOR AND        MEANS FOR ADJUSTING THE FIRING STROKE OF A FIRING MEMBER, now        U.S. Pat. No. 9,844,374;    -   U.S. patent application Ser. No. 14/574,483, entitled SURGICAL        INSTRUMENT ASSEMBLY COMPRISING LOCKABLE SYSTEMS, now U.S. Pat.        No. 10,188,385;    -   U.S. patent application Ser. No. 14/575,139, entitled DRIVE        ARRANGEMENTS FOR ARTICULATABLE SURGICAL INSTRUMENTS, now U.S.        Pat. No. 9,844,375;    -   U.S. patent application Ser. No. 14/575,148, entitled LOCKING        ARRANGEMENTS FOR DETACHABLE SHAFT ASSEMBLIES WITH ARTICULATABLE        SURGICAL END EFFECTORS, now U.S. Pat. No. 10,085,748;    -   U.S. patent application Ser. No. 14/575,130, entitled SURGICAL        INSTRUMENT WITH AN ANVIL THAT IS SELECTIVELY MOVABLE ABOUT A        DISCRETE NON-MOVABLE AXIS RELATIVE TO A STAPLE CARTRIDGE, now        U.S. Pat. No. 10,245,027;    -   U.S. patent application Ser. No. 14/575,143, entitled SURGICAL        INSTRUMENTS WITH IMPROVED CLOSURE ARRANGEMENTS, now U.S. Pat.        No. 10,004,501;    -   U.S. patent application Ser. No. 14/575,117, entitled SURGICAL        INSTRUMENTS WITH ARTICULATABLE END EFFECTORS AND MOVABLE FIRING        BEAM SUPPORT ARRANGEMENTS, now U.S. Pat. No. 9,943,309;    -   U.S. patent application Ser. No. 14/575,154, entitled SURGICAL        INSTRUMENTS WITH ARTICULATABLE END EFFECTORS AND IMPROVED FIRING        BEAM SUPPORT ARRANGEMENTS, now U.S. Pat. No. 9,968,355;    -   U.S. patent application Ser. No. 14/574,493, entitled SURGICAL        INSTRUMENT ASSEMBLY COMPRISING A FLEXIBLE ARTICULATION SYSTEM,        now U.S. Pat. No. 9,897,000; and    -   U.S. patent application Ser. No. 14/574,500, entitled SURGICAL        INSTRUMENT ASSEMBLY COMPRISING A LOCKABLE ARTICULATION SYSTEM,        now U.S. Pat. No. 10,117,649.

Applicant of the present application owns the following patentapplications that were filed on Mar. 1, 2013 and which are each hereinincorporated by reference in their respective entirety:

-   -   U.S. patent application Ser. No. 13/782,295, entitled        ARTICULATABLE SURGICAL INSTRUMENTS WITH CONDUCTIVE PATHWAYS FOR        SIGNAL COMMUNICATION, now U.S. Pat. No. 9,700,309;    -   U.S. patent application Ser. No. 13/782,323, entitled ROTARY        POWERED ARTICULATION JOINTS FOR SURGICAL INSTRUMENTS, now U.S.        Pat. No. 9,782,169;    -   U.S. patent application Ser. No. 13/782,338, entitled THUMBWHEEL        SWITCH ARRANGEMENTS FOR SURGICAL INSTRUMENTS, now U.S. Patent        Application Publication No. 2014/0249557;    -   U.S. patent application Ser. No. 13/782,499, entitled        ELECTROMECHANICAL SURGICAL DEVICE WITH SIGNAL RELAY ARRANGEMENT,        now U.S. Pat. No. 9,358,003;    -   U.S. patent application Ser. No. 13/782,460, entitled MULTIPLE        PROCESSOR MOTOR CONTROL FOR MODULAR SURGICAL INSTRUMENTS, now        U.S. Pat. No. 9,554,794;    -   U.S. patent application Ser. No. 13/782,358, entitled JOYSTICK        SWITCH ASSEMBLIES FOR SURGICAL INSTRUMENTS, now U.S. Pat. No.        9,326,767;    -   U.S. patent application Ser. No. 13/782,481, entitled SENSOR        STRAIGHTENED END EFFECTOR DURING REMOVAL THROUGH TROCAR, now        U.S. Pat. No. 9,468,438;    -   U.S. patent application Ser. No. 13/782,518, entitled CONTROL        METHODS FOR SURGICAL INSTRUMENTS WITH REMOVABLE IMPLEMENT        PORTIONS, now U.S. Patent Application Publication No.        2014/0246475;    -   U.S. patent application Ser. No. 13/782,375, entitled ROTARY        POWERED SURGICAL INSTRUMENTS WITH MULTIPLE DEGREES OF FREEDOM,        now U.S. Pat. No. 9,398,911; and    -   U.S. patent application Ser. No. 13/782,536, entitled SURGICAL        INSTRUMENT SOFT STOP, now U.S. Pat. No. 9,307,986.

Applicant of the present application also owns the following patentapplications that were filed on Mar. 14, 2013 and which are each hereinincorporated by reference in their respective entirety:

-   -   U.S. patent application Ser. No. 13/803,097, entitled        ARTICULATABLE SURGICAL INSTRUMENT COMPRISING A FIRING DRIVE, now        U.S. Pat. No. 9,687,230;    -   U.S. patent application Ser. No. 13/803,193, entitled CONTROL        ARRANGEMENTS FOR A DRIVE MEMBER OF A SURGICAL INSTRUMENT, now        U.S. Pat. No. 9,332,987;    -   U.S. patent application Ser. No. 13/803,053, entitled        INTERCHANGEABLE SHAFT ASSEMBLIES FOR USE WITH A SURGICAL        INSTRUMENT, now U.S. Pat. No. 9,883,860;    -   U.S. patent application Ser. No. 13/803,086, entitled        ARTICULATABLE SURGICAL INSTRUMENT COMPRISING AN ARTICULATION        LOCK, now U.S. Patent Application Publication No. 2014/0263541;    -   U.S. patent application Ser. No. 13/803,210, entitled SENSOR        ARRANGEMENTS FOR ABSOLUTE POSITIONING SYSTEM FOR SURGICAL        INSTRUMENTS, now U.S. Pat. No. 9,808,244;    -   U.S. patent application Ser. No. 13/803,148, entitled        MULTI-FUNCTION MOTOR FOR A SURGICAL INSTRUMENT, now U.S. Pat.        No. 10,470,762;    -   U.S. patent application Ser. No. 13/803,066, entitled DRIVE        SYSTEM LOCKOUT ARRANGEMENTS FOR MODULAR SURGICAL INSTRUMENTS,        now U.S. Pat. No. 9,629,623;    -   U.S. patent application Ser. No. 13/803,117, entitled        ARTICULATION CONTROL SYSTEM FOR ARTICULATABLE SURGICAL        INSTRUMENTS, now U.S. Pat. No. 9,351,726;    -   U.S. patent application Ser. No. 13/803,130, entitled DRIVE        TRAIN CONTROL ARRANGEMENTS FOR MODULAR SURGICAL INSTRUMENTS, now        U.S. Pat. No. 9,351,727; and    -   U.S. patent application Ser. No. 13/803,159, entitled METHOD AND        SYSTEM FOR OPERATING A SURGICAL INSTRUMENT, now U.S. Pat. No.        9,888,919.

Applicant of the present application also owns the following patentapplication that was filed on Mar. 7, 2014 and is herein incorporated byreference in its entirety:

-   -   U.S. patent application Ser. No. 14/200,111, entitled CONTROL        SYSTEMS FOR SURGICAL INSTRUMENTS, now U.S. Pat. No. 9,629,629.

Applicant of the present application also owns the following patentapplications that were filed on Mar. 26, 2014 and are each hereinincorporated by reference in their respective entirety:

-   -   U.S. patent application Ser. No. 14/226,106, entitled POWER        MANAGEMENT CONTROL SYSTEMS FOR SURGICAL INSTRUMENTS, now U.S.        Patent Application Publication No. 2015/0272582;    -   U.S. patent application Ser. No. 14/226,099, entitled        STERILIZATION VERIFICATION CIRCUIT, now U.S. Pat. No. 9,826,977;    -   U.S. patent application Ser. No. 14/226,094, entitled        VERIFICATION OF NUMBER OF BATTERY EXCHANGES/PROCEDURE COUNT, now        U.S. Patent Application Publication No. 2015/0272580;    -   U.S. patent application Ser. No. 14/226,117, entitled POWER        MANAGEMENT THROUGH SLEEP OPTIONS OF SEGMENTED CIRCUIT AND WAKE        UP CONTROL, now U.S. Pat. No. 10,013,049;    -   U.S. patent application Ser. No. 14/226,075, entitled MODULAR        POWERED SURGICAL INSTRUMENT WITH DETACHABLE SHAFT ASSEMBLIES,        now U.S. Pat. No. 9,743,929;    -   U.S. patent application Ser. No. 14/226,093, entitled FEEDBACK        ALGORITHMS FOR MANUAL BAILOUT SYSTEMS FOR SURGICAL INSTRUMENTS,        now U.S. Pat. No. 10,028,761;    -   U.S. patent application Ser. No. 14/226,116, entitled SURGICAL        INSTRUMENT UTILIZING SENSOR ADAPTATION, now U.S. Patent        Application Publication No. 2015/0272571;    -   U.S. patent application Ser. No. 14/226,071, entitled SURGICAL        INSTRUMENT CONTROL CIRCUIT HAVING A SAFETY PROCESSOR, now U.S.        Pat. No. 9,690,362;    -   U.S. patent application Ser. No. 14/226,097, entitled SURGICAL        INSTRUMENT COMPRISING INTERACTIVE SYSTEMS, now U.S. Pat. No.        9,820,738;    -   U.S. patent application Ser. No. 14/226,126, entitled INTERFACE        SYSTEMS FOR USE WITH SURGICAL INSTRUMENTS, now U.S. Pat. No.        10,004,497;    -   U.S. patent application Ser. No. 14/226,133, entitled MODULAR        SURGICAL INSTRUMENT SYSTEM, now U.S. Patent Application        Publication No. 2015/0272557;    -   U.S. patent application Ser. No. 14/226,081, entitled SYSTEMS        AND METHODS FOR CONTROLLING A SEGMENTED CIRCUIT, now U.S. Pat.        No. 9,804,618;    -   U.S. patent application Ser. No. 14/226,076, entitled POWER        MANAGEMENT THROUGH SEGMENTED CIRCUIT AND VARIABLE VOLTAGE        PROTECTION, now U.S. Pat. No. 9,733,663;    -   U.S. patent application Ser. No. 14/226,111, entitled SURGICAL        STAPLING INSTRUMENT SYSTEM, now U.S. Pat. No. 9,750,499; and    -   U.S. patent application Ser. No. 14/226,125, entitled SURGICAL        INSTRUMENT COMPRISING A ROTATABLE SHAFT, now U.S. Pat. No.        10,201,364.

Applicant of the present application also owns the following patentapplications that were filed on Sep. 5, 2014 and which are each hereinincorporated by reference in their respective entirety:

-   -   U.S. patent application Ser. No. 14/479,103, entitled CIRCUITRY        AND SENSORS FOR POWERED MEDICAL DEVICE, now U.S. Pat. No.        10,111,679;    -   U.S. patent application Ser. No. 14/479,119, entitled ADJUNCT        WITH INTEGRATED SENSORS TO QUANTIFY TISSUE COMPRESSION, now U.S.        Pat. No. 9,724,094;    -   U.S. patent application Ser. No. 14/478,908, entitled MONITORING        DEVICE DEGRADATION BASED ON COMPONENT EVALUATION, now U.S. Pat.        No. 9,737,301;    -   U.S. patent application Ser. No. 14/478,895, entitled MULTIPLE        SENSORS WITH ONE SENSOR AFFECTING A SECOND SENSOR'S OUTPUT OR        INTERPRETATION, now U.S. Pat. No. 9,757,128;    -   U.S. patent application Ser. No. 14/479,110, entitled POLARITY        OF HALL MAGNET TO DETECT MISLOADED CARTRIDGE, now U.S. Pat. No.        10,016,199;    -   U.S. patent application Ser. No. 14/479,098, entitled SMART        CARTRIDGE WAKE UP OPERATION AND DATA RETENTION, now U.S. Pat.        No. 10,135,242;    -   U.S. patent application Ser. No. 14/479,115, entitled MULTIPLE        MOTOR CONTROL FOR POWERED MEDICAL DEVICE, now U.S. Pat. No.        9,788,836; and    -   U.S. patent application Ser. No. 14/479,108, entitled LOCAL        DISPLAY OF TISSUE PARAMETER STABILIZATION, now U.S. Patent        Application Publication No. 2016/0066913.

Applicant of the present application also owns the following patentapplications that were filed on Apr. 9, 2014 and which are each hereinincorporated by reference in their respective entirety:

-   -   U.S. patent application Ser. No. 14/248,590, entitled MOTOR        DRIVEN SURGICAL INSTRUMENTS WITH LOCKABLE DUAL DRIVE SHAFTS, now        U.S. Pat. No. 9,826,976;    -   U.S. patent application Ser. No. 14/248,581, entitled SURGICAL        INSTRUMENT COMPRISING A CLOSING DRIVE AND A FIRING DRIVE        OPERATED FROM THE SAME ROTATABLE OUTPUT, now U.S. Pat. No.        9,649,110;    -   U.S. patent application Ser. No. 14/248,595, entitled SURGICAL        INSTRUMENT SHAFT INCLUDING SWITCHES FOR CONTROLLING THE        OPERATION OF THE SURGICAL INSTRUMENT, now U.S. Pat. No.        9,844,368;    -   U.S. patent application Ser. No. 14/248,588, entitled POWERED        LINEAR SURGICAL STAPLE/FASTENER, now U.S. Pat. No. 10,405,857;    -   U.S. patent application Ser. No. 14/248,591, entitled        TRANSMISSION ARRANGEMENT FOR A SURGICAL INSTRUMENT, now U.S.        Pat. No. 10,149,680;    -   U.S. patent application Ser. No. 14/248,584, entitled MODULAR        MOTOR DRIVEN SURGICAL INSTRUMENTS WITH ALIGNMENT FEATURES FOR        ALIGNING ROTARY DRIVE SHAFTS WITH SURGICAL END EFFECTOR SHAFTS,        now U.S. Pat. No. 9,801,626;    -   U.S. patent application Ser. No. 14/248,587, entitled POWERED        SURGICAL STAPLE/FASTENER, now U.S. Pat. No. 9,867,612;    -   U.S. patent application Ser. No. 14/248,586, entitled DRIVE        SYSTEM DECOUPLING ARRANGEMENT FORA SURGICAL INSTRUMENT, now U.S.        Pat. No. 10,136,887; and    -   U.S. patent application Ser. No. 14/248,607, entitled MODULAR        MOTOR DRIVEN SURGICAL INSTRUMENTS WITH STATUS INDICATION        ARRANGEMENTS, now U.S. Pat. No. 9,814,460.

Applicant of the present application also owns the following patentapplications that were filed on Apr. 16, 2013 and which are each hereinincorporated by reference in their respective entirety:

-   -   U.S. Provisional Patent Application Ser. No. 61/812,365,        entitled SURGICAL INSTRUMENT WITH MULTIPLE FUNCTIONS PERFORMED        BY A SINGLE MOTOR;    -   U.S. Provisional Patent Application Ser. No. 61/812,376,        entitled LINEAR CUTTER WITH POWER;    -   U.S. Provisional Patent Application Ser. No. 61/812,382,        entitled LINEAR CUTTER WITH MOTOR AND PISTOL GRIP;    -   U.S. Provisional Patent Application Ser. No. 61/812,385,        entitled SURGICAL INSTRUMENT HANDLE WITH MULTIPLE ACTUATION        MOTORS AND MOTOR CONTROL; and    -   U.S. Provisional Patent Application Ser. No. 61/812,372,        entitled SURGICAL INSTRUMENT WITH MULTIPLE FUNCTIONS PERFORMED        BY A SINGLE MOTOR.

Numerous specific details are set forth to provide a thoroughunderstanding of the overall structure, function, manufacture, and useof the embodiments as described in the specification and illustrated inthe accompanying drawings. Well-known operations, components, andelements have not been described in detail so as not to obscure theembodiments described in the specification. The reader will understandthat the embodiments described and illustrated herein are non-limitingexamples, and thus it can be appreciated that the specific structuraland functional details disclosed herein may be representative andillustrative. Variations and changes thereto may be made withoutdeparting from the scope of the claims.

The terms “comprise” (and any form of comprise, such as “comprises” and“comprising”), “have” (and any form of have, such as “has” and“having”), “include” (and any form of include, such as “includes” and“including”) and “contain” (and any form of contain, such as “contains”and “containing”) are open-ended linking verbs. As a result, a surgicalsystem, device, or apparatus that “comprises,” “has,” “includes” or“contains” one or more elements possesses those one or more elements,but is not limited to possessing only those one or more elements.Likewise, an element of a system, device, or apparatus that “comprises,”“has,” “includes” or “contains” one or more features possesses those oneor more features, but is not limited to possessing only those one ormore features.

The terms “proximal” and “distal” are used herein with reference to aclinician manipulating the handle portion of the surgical instrument.The term “proximal” refers to the portion closest to the clinician andthe term “distal” refers to the portion located away from the clinician.It will be further appreciated that, for convenience and clarity,spatial terms such as “vertical”, “horizontal”, “up”, and “down” may beused herein with respect to the drawings. However, surgical instrumentsare used in many orientations and positions, and these terms are notintended to be limiting and/or absolute.

Various exemplary devices and methods are provided for performinglaparoscopic and minimally invasive surgical procedures. However, thereader will readily appreciate that the various methods and devicesdisclosed herein can be used in numerous surgical procedures andapplications including, for example, in connection with open surgicalprocedures. As the present Detailed Description proceeds, the readerwill further appreciate that the various instruments disclosed hereincan be inserted into a body in any way, such as through a naturalorifice, through an incision or puncture hole formed in tissue, etc. Theworking portions or end effector portions of the instruments can beinserted directly into a patient's body or can be inserted through anaccess device that has a working channel through which the end effectorand elongate shaft of a surgical instrument can be advanced.

A surgical stapling system can comprise a shaft and an end effectorextending from the shaft. The end effector comprises a first jaw and asecond jaw. The first jaw comprises a staple cartridge. The staplecartridge is insertable into and removable from the first jaw; however,other embodiments are envisioned in which a staple cartridge is notremovable from, or at least readily replaceable from, the first jaw. Thesecond jaw comprises an anvil configured to deform staples ejected fromthe staple cartridge. The second jaw is pivotable relative to the firstjaw about a closure axis; however, other embodiments are envisioned inwhich the first jaw is pivotable relative to the second jaw. Thesurgical stapling system further comprises an articulation jointconfigured to permit the end effector to be rotated, or articulated,relative to the shaft. The end effector is rotatable about anarticulation axis extending through the articulation joint. Otherembodiments are envisioned which do not include an articulation joint.

The staple cartridge comprises a cartridge body. The cartridge bodyincludes a proximal end, a distal end, and a deck extending between theproximal end and the distal end. In use, the staple cartridge ispositioned on a first side of the tissue to be stapled and the anvil ispositioned on a second side of the tissue. The anvil is moved toward thestaple cartridge to compress and clamp the tissue against the deck.Thereafter, staples removably stored in the cartridge body can bedeployed into the tissue. The cartridge body includes staple cavitiesdefined therein wherein staples are removably stored in the staplecavities. The staple cavities are arranged in six longitudinal rows.Three rows of staple cavities are positioned on a first side of alongitudinal slot and three rows of staple cavities are positioned on asecond side of the longitudinal slot. Other arrangements of staplecavities and staples may be possible.

The staples are supported by staple drivers in the cartridge body. Thedrivers are movable between a first, or unfired position, and a second,or fired, position to eject the staples from the staple cavities. Thedrivers are retained in the cartridge body by a retainer which extendsaround the bottom of the cartridge body and includes resilient membersconfigured to grip the cartridge body and hold the retainer to thecartridge body. The drivers are movable between their unfired positionsand their fired positions by a sled. The sled is movable between aproximal position adjacent the proximal end and a distal positionadjacent the distal end. The sled comprises a plurality of rampedsurfaces configured to slide under the drivers and lift the drivers, andthe staples supported thereon, toward the anvil.

Further to the above, the sled is moved distally by a firing member. Thefiring member is configured to contact the sled and push the sled towardthe distal end. The longitudinal slot defined in the cartridge body isconfigured to receive the firing member. The anvil also includes a slotconfigured to receive the firing member. The firing member furthercomprises a first cam which engages the first jaw and a second cam whichengages the second jaw. As the firing member is advanced distally, thefirst cam and the second cam can control the distance, or tissue gap,between the deck of the staple cartridge and the anvil. The firingmember also comprises a knife configured to incise the tissue capturedintermediate the staple cartridge and the anvil. It is desirable for theknife to be positioned at least partially proximal to the rampedsurfaces such that the staples are ejected ahead of the knife.

FIGS. 1 and 2 depict a surgical instrument assembly 1000 comprising asensing system configured to sense a parameter such as displacement, forexample, of an actuation member of the surgical instrument assembly1000. The surgical instrument assembly 1000 comprises a shaft assembly1010 and an end effector assembly 1030 attached to the shaft assembly1010 by way of an articulation joint 1020. The shaft assembly 1010comprises an attachment portion 1011 configured to be attached to anattachment interface. Such an attachment interface may comprise, forexample, a surgical robot and/or a handheld surgical device. The shaftassembly 1010 further comprises a body portion 1013 configured to houseinternal components of the surgical instrument assembly 1000. The endeffector assembly 1030 comprises a proximal frame portion 1031 attachedto the shaft assembly 1011 by way of the articulation joint 1020. Theend effector assembly 1030 further comprises a first jaw 1032 and asecond jaw 1033. The end effector assembly 1030 comprises a surgicalstapling end effector; however, other types of surgical end effectorsare contemplated.

The surgical instrument assembly 1000 further comprises an actuationsystem 1050 configured to actuate a function of the end effectorassembly 1030. The actuation system 1050 comprises a first actuationmember 1051 configured to be operably coupled with an actuation driverof the attachment interface to actuate the function of the end effectorassembly 1030. The actuation system 1050 further comprises a secondactuation member 1055 coupled to the first actuation member 1051 suchthat the first actuation member 1051 can move the second actuationmember 1055. The second actuation member 1055 comprises a proximal end1056 comprising a tab 1057 extending into a slot 1053 of the firstactuation member 1051. The second actuation member 1055 extends throughthe articulation joint 1020 and into the end effector assembly 1030. Thesecond actuation member 1055 comprises a knife body 1059 configured tobe actuated through the end effector assembly 1030 during a firingstroke. The second actuation member 1055 comprises a flexibleconfiguration such that the second actuation member 1055 can be actuatedwhen the surgical instrument assembly 1000 is in an articulatedconfiguration. While a surgical stapling actuation member is depicted,other longitudinally translatable surgical actuation members arecontemplated.

The surgical instrument assembly 1000 further comprises a sensing system1060 configured to sense a parameter of the actuation system 1050. Thesensing system 1060 comprises a stretchable optical waveguide 1061comprising a proximal end 1063 fixed to the shaft 1013 relative to theactuation system 1050 and a distal end 1065 fixed to a tab 1058 of thesecond actuation member 1055. The stretchable optical waveguide 1061extends across the articulation joint 1020. The stretchable opticalwaveguide 1061 is configured to stretch as the second actuation member1055 is moved distally through the firing stroke. The tab 1058 isconfigured to pull the stretchable optical waveguide 1061 and stretchthe stretchable optical waveguide as the second actuation member 1055 isadvanced distally through the firing stroke. In at least one instance,the stretchable optical waveguide 1061 is held in tension in its homeposition.

The sensing system 1060 further comprises an attachment point 1064. Thestretchable optical waveguide 1061 comprises a PDMS optical waveguideattached at the attachment point 1064. The stretchable optical waveguide1061 comprises a light sensor that utilizes light emission within theoptical wave guide and light measuring devices to measure thetransmission of light through the waveguide as the waveguide stretches.In at least one instance, light is provided by vertical-cavitysurface-emitting lasers. Such light measuring devices may comprise, forexample, photodiodes. As the stretchable optical waveguide 1061 isstretched, the loss of light transmission within the stretchable opticalwaveguide 1061 increases. This difference in light transmission withinthe stretchable optical waveguide 1061 can be detected by thephotodiodes. Similarly, as the stretchable optical waveguide 1061returns to its un-stretched or, home, position, the amount of lighttransmitted within the stretchable optical waveguide 1061 increases.

The surgical instrument assembly 1000 further comprises a controlcircuit configured to monitor the light transmission through thestretchable optical waveguide 1061 by monitoring the signals transmittedby the photodiodes. In at least one instance, the stretchable opticalwaveguide 1061 comprises a single output corresponding to the stretchlength of the stretchable optical waveguide 1061. The control circuit isconfigured to determine a parameter, such as displacement, for example,of the knife body 1059 based on the monitored light transmission withinthe stretchable optical waveguide 1061. In such instances, the signalsreceived from the photodiodes correspond to the position of the knifebody 1059. The position of the knife body 1059 can be determined bycomparing the monitored signals to a pre-determined data set and/or by apre-determined algorithm. In addition to the above, monitoring thesignals of the photodiodes over time can allow the tracking ofparameters involving time. Such parameters include acceleration andvelocity, for example.

In at least one instance, the control circuit is configured to measurethe light transmission, or optical loss, within the stretchable opticalwaveguide 1061 when the actuation system 1050 is in an unfiredconfiguration. The control circuit can subsequently compare the measuredlight transmission within the stretchable optical waveguide1061 to thelight transmission measured in the unfired configuration to determinethe position of the knife body 1059 relative to the unfired position ofthe knife body 1059. The position of the knife body 1059 can then bedetermined based on the change in light transmission within thestretchable optical waveguide 1061 as a function of the stretch lengthof the stretchable optical waveguide 1061.

In at least one instance, the control circuit is configured to comparethe determined displacement of the knife body 1059 to an expecteddisplacement of the knife body 1059 deduced by a motor encoder on themotor driving the actuation system 1050. In at least one instance, thecontrol circuit is configured to adjust the control program of theactuation system 1050 if there are discrepancies between themotor-encoder data and the sensed displacement by way of the sensingsystem 1060. A discrepancy between the two systems could indicate thatthere is system backlash, for example, between the motor and the knifebody 1059. Such detected variance can be corrected for by the controlcircuit to ensure a full firing stroke, for example.

In at least one instance, surgical instruments comprising can comprisemultiple stretchable optical waveguides. For example, the articulationsystem may comprise a stretchable optical waveguide and/or a separateclosure system may comprise a stretchable optical waveguide. Thewaveguides may be attached at any suitable location on the drive membersand at any suitable location on the shaft. In at least one instance, astretchable optical waveguide is attached to two non-fixed attachmentlocations. For example, a waveguide may be attached to a knife body andan articulation drive rod. In such an instance, the difference inactuation length of each member may vary substantially enough to be ableto use a stretchable optical waveguide in such a manner.

A control system receiving data regarding the actual position of astaple firing drive, a closure drive, and/or an articulation drive canmodify the actuation strokes of these drives after evaluating the data.For instance, if the control system detects that the staple firing driveis further distal than anticipated, the control system can shorten theactuation stroke of the staple firing drive.

FIG. 3 depicts a surgical instrument assembly 1100 comprising a sensingsystem configured to sense a parameter of an actuation member of thesurgical instrument assembly 1100. The surgical instrument assembly 1100is similar in many respects to the surgical instrument assembly 1000discussed above. The surgical instrument assembly 1100 comprises asensing system 1160 configured to sense a parameter of the actuationsystem 1050. The sensing system 1160 comprises a stretchable opticalwaveguide 1161 comprising a proximal end 1163 fixed to the shaft 1013relative to the actuation system 1050 and a distal end 1165 fixeddirectly to the knife body 1059. The stretchable optical waveguide 1161extends across the articulation joint 1020. The stretchable opticalwaveguide 1161 is configured to stretch as the second actuation member1055 is moved through the firing stroke. The knife body 1059 isconfigured to pull the stretchable optical waveguide 1161 and stretchthe stretchable optical waveguide 1161 as the second actuation member1055 is advanced distally through the firing stroke. In at least oneinstance, the stretchable optical waveguide 1161 is held in tension inits home position.

Referring to FIG. 3, further to the above, distances 1171, 1173, 1175are labeled and correspond to various positions of the knife body 1059along its staple firing stroke. Distance 1171 corresponds to a homeposition of the knife body 1059, distance 1173 corresponds to anintermediate position of the knife body 1059, and distance 1175corresponds to an end-of-stroke position of the knife body 1059. Thesedistances 1171, 1173, 1175 correspond to magnitudes of lighttransmission sensed within the stretchable optical waveguide 1161. Ifthe light sensed within the optical waveguide 1161 matches the expectedlight within the optical waveguide 1161 for a given position of theknife body 1059, the control system does not modify the stroke length ofthe knife body 1059. If, however, the light sensed within the opticalwaveguide 1161 does not match the expected light within the opticalwaveguide 1161, the control system can shorten or lengthen the strokelength of the knife body 1069 such that the knife body 1059 stops at thecorrect location at the end of the firing stroke. In addition to or inlieu of the above, the control system can modify another parameter ofthe firing stroke based on the light sensed within the optical waveguide1161. For instance, the control system can alter the speed and/oracceleration of the knife body 1059 when the sensed light intensitywithin the optical waveguide 1161 does not match the expected lightintensity. For example, the control system can lower the maximum speedof the knife body 1059 and/or lower the maximum acceleration of theknife body 1059 when the sensed and expected light intensities don'tmatch. In many instances, a slower knife body 1059 is less likely tocause unexpected damage to the stapling system that might be caused by ashifted knife body 1059. Also, for example, the control system can lowerthe maximum current that can be drawn by the electric motor when thesensed and expected light intensities don't match. In such instances,the force transmitted through the knife body 1059 is lowered to reduceto possibility of unexpected damage to the stapling system. In certaininstances, the control system can modify the time, or pause, betweenoperational steps when a discrepancy is detected. In at least oneinstance, the control system can increase the pause between clamping theend effector and performing a staple firing stroke, for example.

FIGS. 4-6 depict a surgical instrument assembly 1200 comprising asensing system configured to sense a parameter of an actuation member ofthe surgical instrument assembly 1200. The surgical instrument assembly1200 is similar in many respects to the surgical instrument assemblies1000, 1100 discussed above. The surgical instrument assembly 1200comprises a sensing system 1260 configured to sense a parameter of theactuation system 1050. The sensing system 1260 comprises a stretchableoptical waveguide 1261 comprising a proximal end 1263 fixed to theproximal frame portion 1031 (distal to the articulation joint 1020) ofthe end effector assembly 1030 relative to the actuation system 1050 anda distal end 1265 fixed directly to the knife body 1059. The sensingsystem 1260 further comprises an electrical connection 1280 attached tothe sensing system 1260 configured to transmit signals to a controlcircuit. The stretchable optical waveguide 1261 does not extend acrossthe articulation joint 1020. The stretchable optical waveguide 1261 isconfigured to stretch as the knife body 1059 is moved through the firingstroke. The knife body 1059 is configured to pull the stretchableoptical waveguide 1261 and stretch the stretchable optical waveguide1261 as the second actuation member 1055 is advanced distally throughthe firing stroke.

FIG. 4 illustrates the stretchable optical waveguide 1261 in its homeconfiguration indicating that the knife body 1059 is at its homeposition 1271. In at least one instance, the stretchable opticalwaveguide 1261 is held in tension in its home configuration. FIG. 5illustrates the stretchable optical waveguide 1261 in a stretchedconfiguration indicating that the knife body 1059 is at an end-of-strokeposition 1275. FIG. 6 illustrates the surgical instrument assembly 1200in an articulated configuration where the electrical connection is bentaround the articulation joint to accommodate the articulatedconfiguration. As can be seen in FIG. 6, the stretchable opticalwaveguide 1261 is not affected by the articulation of the end effectorassembly 1030.

In at least one instance, a control circuit is configured to determinewhen the knife body 1059 reaches position 1273 (FIG. 4). Once the knifebody 1059 reaches the position 1273, the control circuit can dynamicallybreak the motor driving the knife body 1059 to prevent the knife body1059 from crashing into the end of the end effector assembly 1030. Suchcrashing may cause damage to the knife body 1059 and/or componentswithin the surgical instrument assembly 1200 to seize and/or jam. In atleast one instance, the control system can dynamically brake the knifebody 1059 using a pulse width modulation (PWM) circuit which shortensthe voltage pulses being applied to the electric motor. In otherinstances, a frequency modulation (FM) circuit can be used, for example.In certain instances, the magnitude of the voltage being applied to theelectric motor is lowered. In some instances, the control system canapply reverse polarity pulses to the electric motor to slow the firingstroke. In any event, the information provided by the waveguide 1261 tothe control system allows the control system to determine when to beginthe braking process. In at least one instance, the staple firing strokeis 60 mm long, for example, and the control system is configured tobegin its braking routine at the 50 mm location in the staple firingstroke. If the control system detects that the light intensity detectedby the waveguide 1261 does not match the predicted light intensity for agiven distance in the staple firing stroke, the control system may beginits braking process earlier than 50 mm, for example.

Further to the above, the control system can be configured to assesswhether the measured light within a waveguide is within a certainacceptable range. In such instances, the control system will determinethat a match has been made and will not alter the firing stokecharacteristics, at least based on this type of measurement. If,however, the measured light falls outside of the acceptable range, thecontrol system can modify the firing strike as described herein.

The stretchable optical waveguide 1261 is configured to stretch within achannel in the first jaw 1032 as the knife body 1059 is advanced.Embodiments are contemplated where the stretchable optical waveguide1261 is positioned to stretch within the second jaw 1033. In at leastone instance, the stretchable optical waveguide 1261 can be used todetermine the position of the first jaw 1032 relative to the second jaw1033. For example, in surgical stapling end effector assemblies, theknife body 1059 is used to clamp the first jaw 1032 relative to thesecond jaw 1033. In such assemblies, longitudinal travel of the knifebody 1059 can also determine the state of clamping of the end effectorassembly 1030. Another example can involve a separate clamping actuator;however, when the end effector assembly is clamped, the knife body 1059is pulled and/or pushed forward slightly into a ready-to-fire position.This movement, caused by the clamping actuator, can be detected by thestretchable optical waveguide 1261.

FIGS. 7A and 7B depict a surgical instrument assembly 1300 configured todetect a parameter of an actuation member of the surgical instrumentassembly 1300. The surgical instrument assembly 1300 comprises a hollowshaft 1310, an actuation member 1320 such as a firing member, forexample, and a sensing system 1330 configured to sense a parameter suchas movement, for example, of the actuation member 1320. The sensingsystem 1330 comprises a plurality of light emitters 1331 orientedperpendicular to or at least substantially perpendicular to theactuation member 1320 and mounted to the hollow shaft 1310, a pluralityof windows 1321 defined in the actuation member 1320 configured to allowlight to pass through the actuation member 1320 and a plurality of lightsensors, or receivers, 1333 configured to detect light emitted by thelight emitters 1331 and mounted to the hollow shaft 1310.

As the actuation member 1320 translates within the hollow shaft 1310,the light sensors 1333 detect the change in light presence caused by thewindows 1321. This change in light presence corresponds to movement ofthe actuation member 1320. Providing multiple light sensors 1333longitudinally along the shaft 1310 allows the detection of changes inlight presence along a length within the shaft 1310. A control circuitcan monitor the signals of each light sensor and determine the exactposition of the actuation member 1320. The control circuit can furthermonitor these signals over time to determine other parameters such as,for example, velocity and acceleration of the actuation member 1320.

In at least one instance, the light sensors 1333 comprise photodiodes.In at least one instance, the light emitters 1331 comprise LEDs. Anysuitable light sensor and/or light emitter can be used. Moreover, anysuitable combination of light sensor and light emitter can be used. Inat least one instance, the detection of light presence, alone, is usedto determine the position of the actuation member 1320. In at least oneinstance, the detection of light intensity is used to determine theposition of the actuation member 1320. Light intensity can be varied byarranging the plurality of windows 1321 in specific patterns where somepatterns allow a first amount of light to pass through and otherpatterns allow a second amount of light to pass through which isdifferent than the first amount of light. Such a sensing systemutilizing lights may provide a greater degree of reliability in aqueousenvironments. For example, light presence detection may be more reliablewhere bodily fluid and/or debris may be present within the range of thesensing system 1330.

Still referring to FIGS. 7A and 7B, a control circuit can compare theposition of the actuation member 1320 detected by the sensing system1330 with an expected position of the actuation member 1320 detected bya motor encoder driving the actuation member 1320. Adjustments can bemade to the motor control program and/or alerts can be sent to a userindicating that a variance exists between the outputs of each detectionsystem.

In various instances, one or more parameters of drive members in asurgical instrument assembly can be sensed using a stretchable resistivematerial in a similar fashion to the stretchable optical waveguidediscussed above.

FIG. 8 depicts a surgical instrument assembly 1400 comprising a shaft1410, an actuation member 1420, and a sensing system 1430 configured tosense a parameter such as, for example, the displacement of theactuation member 1420. The sensing system 1430 comprises a first HallEffect sensor 1431 positioned with the shaft 1410, a second Hall Effectsensor 1433 positioned with the shaft 1410, and a magnet 1435 attachedto the actuation member 1420. The first Hall Effect sensor 1431 isproximal to the second Hall Effect sensor 1433. The magnet 1435 isconfigured to alter the magnetic field surrounding the first Hall Effectsensor 1431 and the second Hall Effect sensor 1433 allowing a controlcircuit to determine the position of the actuation member 1420.

FIG. 9 is graph 1401 of the position of the actuation member 1420relative to the motor position. The motor position can be detected usingan encoder, for example. FIG. 10 is a graph 1402 of the expected voltageof the Hall Effect sensors 1431, 1433 relative to the motor position.FIG. 11 is a graph 1403 including graphs 1401, 1402 as well as theactual readout of the Hall Effect sensors 1431, 1433 during an actuationstroke. The actual readout of the Hall Effect sensors 1431, 1433 differsfrom the expected readout of the Hall Effect sensors 1431, 1433. Thismay be attributed to component wear, for example. Because the actualreadout of the Hall Effect sensors 1431, 1433 differs from the expectedreadout of the Hall Effect sensors 1431, 1433, a control circuit candetect this difference and adjust a motor control program actuating theactuation member 1420 to correct the position of the actuation member1420 relative to the sensing system 1430 and/or otherwise alter theoperation of the motor control program. In various instances, the motorcontrol program can slow the actuation member 1420, shorten the strokeof the actuation member 1420, and/or reduce the maximum current that canbe drawn by the electric motor, for example. In certain instances, thecontrol system can modify the time, or pause, between operational stepswhen a discrepancy is detected. In at least one instance, the controlsystem can increase the pause between clamping the end effector andperforming a staple firing stroke, for example. In addition to or inlieu of the above, the control circuit can ignore the sensing system1430 and rely only on the motor encoder when the expected readoutdiffers from the actual readout.

In various embodiments, further to the above, the distance between theHall Effect sensors 1431 and 1433 is fixed and known to the controlsystem of the surgical instrument. In many instances, the magnet 1435will simultaneously disturb the fields produced by the Hall Effectsensors 1431 and 1433. If the magnet 1435 is closer to the Hall Effectsensor 1431 than the Hall Effect sensor 1433, for instance, thedisturbance detected by the Hall Effect sensor 1431 may be greater thanthe disturbance detected by the Hall Effect sensor 1433. In at least oneinstance, the relative disturbances detected by the Hall Effect sensors1431 and 1433 can be used by the control system to determine and verifythe position of the actuation member 1420. If one or both of thesesensors is producing an output that does not match the expected outputfor a given output of the electric motor, the control system can enterinto a remedial state in which the data input streams are prioritized.

In at least one instance, a control circuit is configured to monitor themovement of a motor and the movement of an actuator configured to beactuated by the motor. The control circuit is configured to compare themonitored movements and take action accordingly. FIG. 12 is a graphillustrating a relationship between a motor and an actuator configuredto be actuated by the motor. The control circuit is configured to movethe actuator through a 60 mm stroke, for example, although any suitablestroke lengths could be used. For instance, a 30 mm stroke or a 45 mmstroke could be used. Movement of the motor 1510 is directly monitoredby a motor encoder. Movement of the actuator 1520 is directly monitoredby any suitable sensing systems such as those discussed herein, forexample. In this instance, the actuator movement is sensed by astretchable optical waveguide. The graph 1510 illustrates sensed motormovement by a motor encoder relative to time. This measurement is localto the motor. The graph 1520 illustrates sensed movement of the actuatorby the stretchable optical waveguide relative to time. This measurementis local to the actuator. In at least one instance, the actuator isdownstream one or more modular attachment location in a modular surgicalinstrument system. For instance, a first measurement can be taken in afirst component of the modular instrument system while a secondmeasurement can be taken in a second component attached to the firstcomponent wherein the attachment between the first and second componentsis either direct or indirect.

The control circuit is configured to run the motor to actuate theactuator. At position A, the control circuit determines that the motorhas been actuated a specific amount corresponding to an expected 50 mmof movement of the actuator. As can be seen at position A, the actuatorhas not traveled the expected 50 mm because the stretchable opticalwaveguide has not sensed 50 mm of movement, yet. At position B, theactuator has been sensed by the stretchable optical waveguide to havemoved 50 mm and the motor has been actuated more than the specificamount corresponding to the expected 50 mm of movement of the actuator.This new amount, seen at position D, can be logged by the controlcircuit to calibrate the motor control program such that this new amountof motor movement corresponds to the expected 50 mm of movement of theactuator from this point forward. This data may also simply be loggedand taken into consideration in subsequent actuations.

Once the actual movement of the actuator is sensed at the 50 mm location(B), the control circuit is configured to extrapolate a new 60 mm target(E). At such point, the control circuit is configured to re-calibratethe 50 mm and 60 mm targets for the motor movement. Once the new targetsD and E are logged, the control circuit can run the motor until the bothsensed movements of the motor and the actuator reach the target (C, E).This calibration can be done for each modular attachment and for eachactuation of a surgical instrument attachment. The control circuit isconfigured to compensate for varied actuation that may be caused by divetrain slop, backlash, and/or wear, for example.

In at least one instance, predefined parameters for a motor such as theinertia of a rotor, for example, could be measured and/or calibrated aspart of the initial assembly of a modular attachment to a motor. Such aparameter can be measured during a dynamic breaking event which slowsthe motor down to prevent inadvertent overstressing of components as anactuation member approaches an end-of-stroke position (such as thebeginning or end of the stroke). Such a parameter can also be measuredduring the acceleration of the motor (such as starting a stroke and/orre-starting a stroke, for example). During such an event, a controlcircuit can utilize a motor encoder to monitor the inertia of the rotorand a local sensing system within the shaft to determine a correspondinginertia of the rotor. If a difference is detected between the determinedinertia values based on the motor encoder and the local sensing systemwithin the shaft given the predefined parameters, the system couldadjust the dynamic braking and/or acceleration of the motor (rate,initiation trigger, magnitude) to have more efficient motor control withthe attached surgical instrument.

In various instances, surgical instrument attachments configured to beattached to surgical instrument control interfaces such as a surgicalrobot, for example, comprise onboard electronics. The onboardelectronics can comprise any suitable circuitry elements such assensors, printed circuit boards, processors, and/or batteries, forexample. Referring now to FIGS. 13-15, a surgical instrument assembly2000 is depicted. The surgical instrument assembly 2000 comprises ashaft 2010, an articulation joint 2011, and an end effector 2020attached to the shaft 2010 by way of the articulation joint 2011. Theend effector 2020 is configured to be articulated relative to the shaft2010 about the articulation joint 2011. The surgical instrument assembly2000 further comprises an articulation actuator 2013 configured toarticulate the end effector 2020.

Still referring to FIGS. 13-15, the surgical instrument assembly 2000further comprises a first flex circuit 2030 attached to the articulationactuator 2013 and a second flex circuit 2040 attached to anotheractuator of the surgical instrument assembly 2000 such as a firingmember, for example. The first flex circuit 2030 extends through theshaft 2010 from a proximal end where the first flex circuit 2030 may beelectrically coupled with contacts of the surgical control interface.The second flex circuit 2040 extends through the shaft 2010 from theproximal end where the second flex circuit 2040 may also be electricallycoupled with the contacts of the surgical control interface.

The first flex circuit 2030 comprises a non-stretchable zone 2031 and astretchable zone 2035. The stretchable zone 2035 comprises stretchableprinted copper attached to printed circuit board 2033 at both ends ofthe stretchable zone 2035. The printed circuit board 2033 may beattached to the first flex circuit 2030 in a proximal location andattached to the articulation actuator 2013 in a distal location. Thenon-stretchable zone 2031 is configured to act as a normal flex circuitand the stretchable zone 2035 is configured to elastically stretchwithin the shaft 2010. The first flex circuit 2030 may be connected tovarious sensors, for example, positioned on the articulation actuator2013 which are configured to measure a parameter of the articulationactuator 2013. The stretchable zone 2035 is configured elongate as thearticulation actuator 2013 is moved through an articulation stroke whilemaintaining an electrical connection between the sensors of thearticulation actuator and an upstream electrical circuit.

The second flex circuit 2040 comprises a non-stretchable zone 2041 and astretchable zone 2045. The stretchable zone 2045 comprises stretchableprinted copper attached to printed circuit board 2043 at both ends ofthe stretchable zone 2045. The printed circuit board 2043 is attached tothe second flex circuit 2040 in a proximal location and is attached tothe firing member in a distal location across the articulation joint2011. The non-stretchable zone 2041 is configured to act as a normalflex circuit and the stretchable zone 2045 is configured to elasticallystretch within the shaft 2010 across the articulation joint 2011. Thestretchable zone 2045, in this instance, may be referred to as anarticulation section of the second flex circuit 2040. The second flexcircuit 2040 may be connected to various sensors, for example,positioned on the firing member and/or within the end effector 2020which are configured to measure one or more parameters of the endeffector. The stretchable zone 2045 is configured to stretch as the endeffector 2020 is articulated about the articulation joint 2011 whilemaintaining an electrical connection between the sensors of the endeffector 2020 and/or firing member and an upstream electrical circuit.The stretchable zone 2045 is also be configured to stretch, or elongate,as the firing member is advanced within the end effector 2020 should thesecond flex circuit 2040 be attached directly to the firing member.

In at least one instance, the first flex circuit 2030 and the secondflex circuit 2040 are configured to elastically rebound and resilientlyassume neutral, un-stretched configurations. Once in the neutralconfigurations, the first flex circuit 2030 and the second flex circuit2040 may be stretched again upon the actuation of various actuatorswithin the surgical instrument assembly 2000.

In at least one instance, the stretchable zones comprise flexibleconductive inks and the non-stretchable zones comprise conductivemetallic traces.

In at least one instance, a configuration is provided that ensures thestretchable zones re-assume the proper neutral configuration after theload which stretched the stretchable zones is relaxed. FIGS. 16-18depict a flex circuit 2100 comprising non-stretchable zones 2110 and astretchable zone 2120 positioned between the non-stretchable zones 2110.The stretchable zone 2120 comprise a plurality of elastic strut, orconnection, members 2130 attaching portions of the flex circuit 2100within the stretchable zone 2120 together. FIG. 16 illustrates thestretchable zone 2120 in a relaxed state. In such a state, the elasticstrut members 2130 and the stretchable zone 2120 of the flex circuit2100 are in a neutral, un-loaded state. In at least one instance, theelastic strut members 2130 are configured to be in tension in theneutral, un-loaded state. Once the stretchable zone 2120 is stretched(FIG. 17), the elastic strut members 2130 are also stretched in the samedirection and orientation that the stretchable zone 2120 is stretched.In this stretched state, the elastic strut members 2130 can ensure theintegrity of the stretchable zone 2120 by carrying at least some of theforce load and controlling the relative positioning of the zones. Whenthe load that is stretching the stretchable zone 2120 is relaxed, thestretchable zone 2120 can be encouraged to its original neutral,un-loaded state (FIG. 18) by the elastic strut members 2130. In at leastone instance, the elastic strut members 2130 can be used to ensure thatthe stretchable zone 2120 is not overstretched.

As can be seen in FIGS. 16-18, the elastic strut members 2130 areoriented in the same direction along a predetermined stretcheddirection. The elastic strut members 2130 may comprise a material andconstruction that is designed to only stretch in the intended stretchdirection to increase the predictability of the elastic strut members2130. In at least one instance, the elastic strut members 2130 areoriented in a crisscross configuration. Such a configuration mayincrease the tensile force provided by the elastic strut members 2130.

In at least one instance, as described in greater detail herein, astretchable zone of a flex circuit can be used to measure a parameter ofan actuator. For example, the stretchable zone can be attached to afixed location and an actuator such that the actuator stretches thestretchable zone as the actuator is actuated. A sensor arrangement, suchas a Hall Effect sensor positioned at on the fixed attachment, or index,location and a magnet positioned on the actuator attachment location,for example, can be used to measure displacement, for example, of theactuator as the actuator moves through an actuation stroke.

In various instances, surgical instrument assemblies comprise a flexcircuit attached to a fixed location of a shaft of the surgicalinstrument assembly and one or more locations of an actuation member ofthe surgical instrument assembly. The flex circuit can comprise one ormore sections extending from the portion fixed to the shaft which wraparound the shaft in a coiled pattern. One section wrapped around theshaft is wrapped around the shaft a half turn more than the othersection so that it extends in the opposite direction from the othersection. The flex circuit is spring biased into the coiled pattern. Theflex circuit is configured to be pulled by the actuator to unwraprelative to the shaft and stretch across a length of the shaft. When theload on the flex circuit is relaxed, the flex circuit is configured tore-wrap itself around the shaft back into its coiled pattern. In atleast one instance, the shaft is configured to translate to actuate afunction of the surgical instrument assembly. In various instances, theshaft is rotatable and/or articulatable and, in other instances, theshaft is fixed.

In various instances, joints within a surgical instrument assembly suchas an articulation joint and/or a rotation joint where multiple drivemembers are connected to each other comprise means for protecting wiringharnesses and/or flex circuits, for example, extending through and/oraround the joints. The wiring harnesses are protected from inducedstress and strains through the full range of motion of the joints. In atleast one instance, the wiring harness comprises a pre-bent section thatextends through an articulation joint. In such an instance, the pre-bentsection is formed in a manner in anticipation of how the wiring harnesswill react as an end effector is articulated about the articulationjoint.

FIGS. 19 and 20 depict a surgical instrument assembly 2200 comprising ashaft 2201 and a flex circuit, or wiring harness, 2210 extending throughthe shaft 2201. The flex circuit 2210 comprises a pre-bent section 2220configured to be positioned near a joint within the surgical instrumentassembly 2200. In at least one instance, the pre-bent configuration ofthe pre-bent section 2220 provides slack in a manner that accommodatesthe bending of components around the joint near which the pre-bentsection 2220 is positioned. In at least one instance, the pre-bentsection 2220 provides space for components. In at least one instance,the pre-bent section 2220 comprises one or more portions fixed tocomponents of the surgical instrument assembly 2200 at and/or near thejoint. In at least one instance, the pre-bent section 2220 is configuredto be flexed, or bent, by the components to which it is attached as thecomponents are actuated within the surgical instrument assembly 2200.

As can be seen in FIG. 20, the pre-bent section 2220 of the flex circuit2210 resides in multiple flex-circuit profile planes 2221. A flexcircuit profile plane is considered to be a plane defined by a substratelayer of the flex circuit itself. In at least one instance, the flexcircuit 2210 is configured to only substantially bend in a flex circuitbend plane. As can be seen in FIGS. 19 and 20, the pre-bent section 2220of the flex circuit 2210 comprises multiple bends in the flex circuitbend plane. In at least one instance, the flex circuit 2210 can bendslightly outside of the flex circuit bend plane.

FIGS. 21 and 22 depict a surgical instrument assembly 2300 comprising ashaft 2301 and a flex circuit, or wiring harness, 2310 extending throughthe shaft 2301. The flex circuit 2310 comprises a pre-bent section 2320configured to be positioned near a joint within the surgical instrumentassembly 2300. In at least one instance, the pre-bent configuration ofthe pre-bent section 2320 provides slack in a manner that accommodatesthe bending of components around the joint near which the pre-bentsection 2320 is positioned. In at least one instance, the pre-bentsection 2320 provides space within the shaft for other components in theshaft. In at least one instance, the pre-bent section 2320 comprises oneor more portions fixed to components of the surgical instrument assembly2300 at and/or near the joint. In at least one instance, the pre-bentsection 2320 is configured to be flexed, or bent, by the components towhich it is attached as the components are actuated within the surgicalinstrument assembly 2200.

As can be seen in FIG. 22, the pre-bent section 2320 of the flex circuit2310 resides in multiple flex-circuit profile planes 2321. A flexcircuit profile plane is considered to be a plane defined by a substratelayer of the flex circuit itself. In at least one instance, the flexcircuit 2310 is configured to only substantially bend in a flex circuitbend plane. As can be seen in FIGS. 21 and 22, the pre-bent section 2320of the flex circuit 2310 comprises multiple bends in the flex circuitbend plane. In at least one instance, the flex circuit 2310 can bendslightly outside of the flex circuit bend plane.

Still referring to FIGS. 21 and 22, the flex circuit 2310 comprises anoff-centered section 2323 which comprises a section of flex circuit thatis off-centered laterally with respect to a shaft axis. Such positioningcan provide space within the shaft for other shaft components in certainareas. In this instance, the pre-bent section 2320 is offset relative tothe shaft axis to bypass on-center drivers 2303. Various surgicalinstrument systems such as surgical stapling end effectors, for example,require on-center drive systems owing to the high operational loadsrequired to fire the surgical stapling end effectors. In such systems,the off-center flex circuit 2310 can provide space for such on-centerdrive systems.

FIGS. 23 and 24 depict a surgical instrument assembly 2400 comprising ashaft 2401 and a flex circuit, or wiring harness, 2410 extending throughthe shaft 2401. The flex circuit 2410 comprises a pre-curved section2420. In at least one instance, the pre-curved section 2420 isconfigured to be positioned near a joint within the surgical instrumentassembly 2400. In at least one instance, the pre-curved section 2420provides space within the shaft for other components. In at least oneinstance, the pre-curved section 2420 is mounted to an inner surface ofthe shaft 2401 such that the pre-curved section 2420 conforms to thetubular shape of the shaft 2401.

As can be seen in FIG. 24, the pre-curved section 2420 of the flexcircuit 2410 resides in a single flex-circuit profile plane 2421. In atleast one instance, this single flex-circuit profile plane 2421 conformsto the tubular shape of the shaft 2401. A flex circuit profile plane isconsidered to be a plane defined by a substrate layer of the flexcircuit itself. In at least one instance, the flex circuit 2410 isconfigured to only substantially bend in a flex circuit bend plane. Ascan be seen in FIGS. 23 and 24, the pre-curved section 2420 of the flexcircuit 2410 is shaped to bend along the tubular shape of the shaft 2401as well as in a flex circuit bend plane which is transverse to theflex-circuit profile plane 2421. Such bending can be advantageous nearan articulation joint to control the movement of the flex circuit 2410within the shaft.

Still referring to FIGS. 23 and 24, the flex circuit 2410 comprises anoff-centered section 2423 which comprises a section of flex circuit thatis off-centered laterally with respect to the longitudinal axis of theshaft. Such positioning can provide space for other shaft components incertain areas. In this instance, the pre-curved section 2420 is offsetrelative to the shaft axis to bypass on-center drivers 2403. Varioussurgical instrument systems such as surgical stapling end effectors, forexample, often require on-center drive systems, i.e., drive systemsoriented along the longitudinal axis of the shaft, owing to the highoperational loads required to fire the surgical stapling end effectors.The flex circuit 2410 can provide space for such on-center drivesystems. In at least one instance, a flex circuit for use in a shaft ofa surgical instrument assembly is configured to bend in multiple planesand directions corresponding to the bending planes of joints and/orcomponents of the surgical instrument assembly.

In at least one instance, the flex circuits are fabricated with pre-bentand/or pre-curved sections such that the pre-bent and/or pre-curvedsections are not required to be bent or curved into this configurationduring use. In various instances, a pre-curved section comprises aportion of the flex circuit that is in a curved configuration when theflex circuit is not under load. Under load, the pre-curved section cancurve further and/or straighten under load.

FIGS. 25-27 depict a surgical instrument assembly 2500 comprising ashaft 2510, an articulation joint 2530, and an end effector 2520attached to the shaft 2510 by way of the articulation joint 2530. Theend effector 2520 is configured to be articulated relative to the shaft2510 with articulation links 2533 coupled to an articulation driver2531. The articulation links are connected to the shaft 2510, the endeffector 2520, and the articulation driver 2531. When the articulationdriver 2531 is actuated, the end effector 2520 is rotated about thearticulation axis AA by way of the articulation links 2533.

The surgical instrument assembly 2500 further comprises a flex circuit2540 extending through the shaft 2510, the articulation joint 2530, andinto the end effector 2520. The flex circuit 2540 can be used for anysuitable electrical connection that is distal to the articulation joint2530. In at least one instance, the flex circuit 2540 comprises fixedattachment points within the shaft 2510 and the end effector 2520. Invarious instances, flex circuits comprise a substantial width and needto be routed through various moving components. The flex circuit 2540comprises a pre-bent section 2541 routed through the articulation joint2530 of the surgical instrument assembly 2500. The flex circuit 2540extends through the articulation links 2533 and comprises an attachmentportion 2543 attached to the articulation driver 2531. As the endeffector 2520 is articulated about the articulation axis AA, thepre-bent section 2543 conforms to the movement of the articulation links2533, the end effector 2520, the articulation driver 2531, and the shaft2510. The articulation driver 2531 is configured to guide the pre-bentsection 2541 by way of the attachment portion 2543 into suitableconfigurations as the end effector 2520 is articulated about thearticulation axis AA. The pre-bent section 2541 permits slack, or slop,proximal to the attachment portion 2543 and distal to the attachmentportion 2543 to prevent any possible strain on the flex circuit 2540.

In at least one instance, the flex circuit 2540 comprises one or moreS-shaped portions. In at least one instance, one or more bends of eachS-shaped portion is fixed to a moving component of the surgicalinstrument assembly 2500. In at least one instance, the flex circuit2540 comprises a plurality of elastic strut members configured to biasthe pre-bent section 2541 into its neutral pre-bent configuration asseen in FIG. 27 when the end effector 2520 is not in an articulatedposition. A flex circuit having integrated moving component supportlocations can provide a greater degree of stability through regions of asurgical instrument assembly that comprises moving regions such asarticulation joints, for example.

FIGS. 28-30 depict a surgical instrument assembly 3000 comprising an endeffector 3001, a firing member 3010, and a sensing system 3030configured to sense a parameter of the firing member 3010. The endeffector 3001 comprises a staple cartridge 3020 including a plurality ofstaples stored therein. The staple cartridge 3020 comprises alongitudinal slot 3021 configured to receive the firing member 3010therein, a tissue-supporting surface, or deck, 3023, a proximal end3025, and a distal end 3027. The firing member 3010 is configured toeject the staples and cut patient tissue compressed against the deck3023 during a staple-firing stroke as the firing member is advanced fromthe proximal end 3025 to the distal end 3027. The firing member 3010comprises a cutting edge 3011, a lower camming member 3013 configured toengage a lower jaw of the end effector 3001, and an upper camming member3014 configured to engage an upper jaw of the end effector 3001.

The sensing system 3030 is configured to sense a parameter such as, forexample, the displacement of the firing member 3010 as the firing member3010 moves within the end effector 3001. The sensing system 3030comprises a magnet 3031 and a plurality of sensors comprising a proximalsensor 3033 positioned on the tissue-supporting surface 3023 at theproximal end 3025 of the staple cartridge 3020 and a distal sensor 3035positioned on the tissue-supporting surface 3023 at the distal end 3027of the staple cartridge 3020. The sensors 3033, 3035 comprise HallEffect sensors; however, any suitable sensor can be used. The magnet3031 is positioned on the front of the firing member 3010. As the firingmember moves through a firing stroke, the signals of the sensors 3033,3035 are configured to fluctuate as the magnet 3031 moves toward andaway from the sensors 3033, 3035. These signals can be used by a controlcircuit to interpret a parameter of the firing member 3010 such asdisplacement, velocity, and/or acceleration, for example. The magnet3031 comprises a proximal limit 3041 (FIG. 29) adjacent the sensor 3033and a distal limit 3043 (FIG. 30) adjacent the sensor 3035.

In at least one instance, a sled of a surgical stapling assembly ismonitored utilizing Hall Effect sensors and magnets, for example. Anysuitable movable actuation member can be sensed within a surgicalinstrument assembly utilizing the sensing system 3033. For example, atranslating member within a bi-polar energy surgical instrument can besensed utilizing the sensing system 3033. In at least one suchembodiment, the translating member comprises a tissue cutting knife, forexample.

In at least one instance, the sensing system 3033 is utilized inconjunction with a control circuit configured to adjust a motor controlprogram. For example, the sensing system 3033 may detect that the firingmember 3010 has not traveled an expected distance compared to amonitored motor movement while the surgical instrument assembly 3000 isin an articulated configuration. This can be due to an increased strokelength of an actuation member configured to move the firing member 3010caused by the actuation member being articulated around an articulationjoint. In such an instance, the control circuit is configured to adjustthe motor control program to compensate for the increased stroke lengthcaused by the articulation of the surgical instrument assembly 3000. Inat least one instance, component wear can cause loss of stroke lengthwithin an actuation system. In such an instance, the control circuit isconfigured to adjust the motor control program to compensate for theloss of stroke length such that a full staple firing stroke canultimately be completed.

FIGS. 31-33 depict a surgical instrument assembly 3100 comprising an endeffector jaw 3101 comprising a staple cartridge channel 3110 configuredto receive a staple cartridge 3140 therein and a sensing system 3130configured to measure a parameter of the surgical instrument assembly3100. The staple cartridge channel 3110 comprises a proximal end 3113, adistal end 3115, and a slot 3111 extending between the proximal end 3113and the distal end 3115 configured to receive a portion of a firingmember therein. The staple cartridge channel 3110 further comprises abottom 3117 configured to support a bottom of the staple cartridge 3140.

The sensing system 3130 is configured to monitor pressure applied to thestaple cartridge 3140. The sensing system 3130 comprises a plurality ofpressure sensors comprising a first set of sensors 3131A positioned on afirst side of the slot 3111 on the bottom 3117 of the cartridge channel3110 and a second set of sensors 3131B positioned on a second side ofthe slot 3111 on the bottom 3117 of the cartridge channel 3110. In atleast one instance, pressure sensors can be positioned on the sides ofthe cartridge channel in addition to or in lieu of sensors positioned onthe bottom 3117 of the cartridge channel 3110. In at least one instance,an anvil jaw can comprise pressure sensors configured to detect pressureapplied to the anvil jaw. In at least one instance, a pressure sensitivefabric and/or conductive thread can be laid on the bottom 3117 of thecartridge channel 3110. In at least one instance, a Velostat sensor canbe used, for example; however, any suitable sensor can be used.

The sensing system 3130 is configured to detect pressure between thestaple cartridge 3140 and the cartridge channel 3110. The sensors 3131A,3131B are connected to a flex circuit 3120 configured to communicate thesignals of the sensors 3131A, 3131B to a control circuit of the surgicalinstrument assembly 3100. The sensing system 3130 is configured tomeasure pressure corresponding to each side of the staple cartridge 3140as well as pressure corresponding to a proximal end 3141 and a distalend 3143 of the staple cartridge 3140. A control circuit is configuredto monitor the pressure sensed by the sensors 3131A, 3131B. In at leastone instance, the control circuit is configured to map out, in realtime, to a user geographically a pressure profile sensed by the sensingsystem 3130. Such a pressure profile can be displayed to a user, forexample. In at least one instance, the control circuit is configured toautomatically adjust a motor control program of a firing member based onsignals received from the pressure sensors 3131A, 3131B. Oftentimes, thetissue compressed between the anvil jaw and the staple cartridge 3140 isnot evenly compressed which creates an uneven pressure profile in thetissue and, in some instances, can affect the staple formation process.The sensors 3131A, 3131B are positioned and arranged to provide thecontrol system with data regarding the pressure profile within thetissue. For instance, the control system can assess whether the tissueis thicker on the first side of the end effector as compared to thesecond side of the end effector. In at least one such instance, thecontrol system is configured to slow down the staple firing stroke whenthe difference between the first side pressure and the second sidepressure exceeds a threshold. In such instances, a slower staple firingstroke can result in better staple formation.

FIGS. 34-37 illustrate a surgical instrument assembly 3200 comprising ahandle 3210, a shaft assembly 3220 extending from the handle 3210, andan end effector 3240 extending from the shaft assembly 3220. The handle3210 comprises a plurality of actuators 3213 configured to be actuatedby a user and a hold-able portion 3211 configured to be held by a user.The actuators 3213 are configured to actuate one or more actuationmembers within the shaft assembly 3220 to actuate a function of the endeffector 3240.

The surgical instrument assembly 3200 further comprises a sensing systemconfigured to detect a parameter of a shaft component 3230 extendingthrough an outer shaft 3221 of the shaft assembly 3220. The shaftcomponent 3230 comprises a plurality of apertures 3231 defined thereinconfigured to slideably receive actuation members therein. In at leastone instance, the shaft component 3230 is configured to experience aload during the actuation of one or more actuation systems within thesurgical instrument assembly 3200. Any suitable component can be sensedby the sensing system. For example, a firing actuator, closure actuator,and/or articulation actuator may be sensed by such a sensing system. Thesensing system comprises a flex circuit 3250 and a sensor 3253 extendingfrom a sensor region 3251 of the flex circuit 3250. The sensor 3253 maycomprise a strain gauge, for example; however, any suitable sensor canbe used. In at least one instance, the flex circuit 3250 extends to theend effector 3240 where additional sensors are positioned and connectedto flex circuit 3250. The shaft component 3230 comprises a channel 3233defined therein within which the flex circuit 3250 is positioned.

In many instances, the measurement of tensile and compression forcesand/or strains transmitted through a drive member is more reliable whenthey are measured toward the central axis of the drive member as opposedto the outer perimeter of the drive member. Stated another way, neckingof the shaft component can also provide a more localized concentrationof stress and strain. To this end, the sensor 3253 is mounted to anecked portion 3235 of the shaft component 3230. A region comprisingsuch necking can provide a more dependable region for a sensor tomeasure a load applied to the shaft component 3230 because even theslightest of load applied to the shaft component 3230 will result in anamplified strain in the necked portion 3235. As can be seen in FIG. 35,the shaft component 3230 is unloaded and the necked portion 3235comprises a first width and the shaft component 3230 comprises a firstlength. In FIG. 36, the shaft component 3230 is loaded and the neckedportion 3235 is elongated resulting in the necked portion 3235comprising a second width that is greater than the first width and theshaft component 3230 comprising a second length that is greater than thefirst length. In at least one instance, the stretching of the shaftcomponent 3230 can be determined by a control circuit interpreting achange in strain values received from the sensor 3253 as the shaftcomponent 3230 is loaded and unloaded.

In various instances, the sensor 3253 does not change the overall shapeand/or properties of the shaft component 3230. In at least one instance,the flex circuit and/or sensors 3253 are embedded in recesses in theshaft component 3230 such that the overall dimension of the shaftcomponent 3230 is not changed by the flex circuit and/or sensors 3253.For instance, the thickness of the flex circuit and/or sensors 3253 isequal to or less than the depth of the recess. Such an arrangement canallow a structural component to maintain its integrity while itsproperties are monitored locally within the shaft assembly 3220.

In at least one instance, strain gauges extending from a flex circuitare attached to several different components within a shaft assembly. Inat least one instance, a portion of a flex circuit extending through ashaft assembly is primarily non-stretchable and another portion of theflex circuit is stretchable. In various instances, the primarilynon-stretchable portion has a higher modulus of elasticity than theother portions of the flex circuit. In at least one instance, themodulus of elasticity of the primarily non-stretchable portion is 10times higher than the modulus of elasticity of the other portions of theflex circuit, for example. In at least one instance, the modulus ofelasticity of the primarily non-stretchable portion is 100 times higherthan the modulus of elasticity of the other portions of the flexcircuit, for example. In at least one instance, the stretchable portionof the flex circuit is used to sense a parameter of a component of ashaft assembly. In at least one instance, the stretchable portion of theflex circuit comprises a substrate material that is thinner than thesubstrate material that makes up the non-stretchable portion. In atleast one instance, the substrate material used for the stretchableportion of the flex circuit is different than the substrate material forthe non-stretchable portion of the flex circuit. In at least oneinstance, conductors within the flex circuit are used as resistiveelements to sense stretch. Such conductors can be used to measure aparameter of a structural component within a shaft assembly and/or endeffector, for example. In at least one instance, a force experienced bya sensed structural member is proportionate to the strain experienced bythe sensed structural member which may be detected using any of themethods disclosed herein.

In at least one instance, a stretchable portion of a flex circuit usedto detect a parameter of a structural member within a shaft assemblycomprises a length that is spread out across the entire length of thestructural member itself so as to maintain a homogenous stretch alongthe length of the structural member. For example, if only a portion ofthe structural member is in contact with a stretchable portion of a flexcircuit, that portion may be strengthened by the additional material ofthe stretchable portion of the flex circuit and this may inadvertentlyfluctuate the sensor readings within that region relative to the regionthat is not in contact with the stretchable portion of the flex circuit.In at least one instance, this is avoided by covering the entire lengthof the structural member with a stretchable flex circuit portion. In atleast one instance, a stretchable flex circuit portion is used tostrengthen a portion of a structural member to be sensed.

In at least one instance, a structural member to be sensed comprisesfeatures to concentrate force experienced by the structural member,direct the force experienced by the structural member in a specificdirection, and/or amplify the load experienced by the structural memberacross its length. In various instances, directing and/or amplifying theflow of strain through a drive member can be accomplished by changes inthe cross-section and/or geometry of the drive member.

In at least one instance, strain experienced by a structural componentof a shaft assembly owing to bending can be sensed by a strain gaugepositioned at the farthest location from the bending axis. Positioningsuch an integrated flex circuit strain gauge can amplify the detectablestress on the bending structural component. In at least one instance,this location is artificially created. An artificially created fin mayextend from a structural component where the fin creates a positionfurther from a bending axis of the structural component than any portionof the structural component itself.

In at least one instance, a control circuit is configured to monitor aparameter of the structural component to be sensed by a sensing systemwithin the shaft assembly and is configured to adjust the operation ofthe surgical instrument assembly in any suitable way, including thosedisclosed herein.

In various instances, the local displacement sensing of a shaftcomponent within a shaft assembly of a surgical instrument assembly canbe used to determine the beginning and end of a stroke of the componentbeing sensed. FIGS. 38-40 depict a surgical instrument assembly 3300comprising a shaft 3310, an articulation joint 3330, an end effector3320 pivotally coupled to the shaft 3310 about the articulation joint3330. The surgical instrument assembly 3300 further comprises a sensingsystem 3340 configured to monitor the displacement of an articulationactuator 3311 configured to articulate the end effector 3320 relative tothe shaft 3310 about an articulation axis AA.

The articulation joint 3330 comprises a first articulation link 3331connected to the articulation actuator 3311 and the shaft 3310 and asecond articulation link 3333 connected to the first articulation link3331 and the end effector 3320. The articulation actuator 3311 isconfigured to be advanced and retracted longitudinally within the shaft3310 to pivot the end effector 3320 about the articulation axis AA. Thefirst articulation link 3331 is pivotally coupled to the shaft 3310, thearticulation actuator 3331, and the second articulation link 3333. Thesecond articulation link 3333 is pivotally coupled to the firstarticulation link 3331 and the end effector 3320.

The sensing system 3340 comprises a sensor 3341 positioned on a distalend 3313 of the articulation actuator 3311, a first magnet 3343positioned on the shaft 3310, and a second magnet 3345 positioned on thesecond articulation link 3333. The sensor 3341 comprises a Hall Effectsensor; however, any suitable sensor and trigger arrangement may beused. For example, an inductive sensor arrangement can be used. Acontrol circuit is configured to monitor signals received by the sensor3341 to determine the exact articulated position of the end effector3320 relative to the shaft 3310. As the articulation actuator 3311 ismoved through an articulation stroke, the sensor 3341 is moved within amagnetic field that is being altered by the magnets 3343, 3345 therebyresulting in a variance of signal of the sensor 3341. This variance insignal can be interpreted by a control circuit by comparing the signalto a range of expected signals and articulated positions to determinethe exact articulated position of the end effector 3320 relative to theshaft 3310.

FIG. 38 illustrates the end effector 3320 in a first articulatedposition where the articulation actuator 3331 is actuated in afully-proximal position. In this configuration, the first magnet 3343 isa first distance d₂₁ from the sensor 3341 and the second magnet 3345 isa second distance d₁₁ from the sensor 3341. A control circuit isconfigured to determine the position of the magnets 3343, 3345 byinterpreting the signal from the Hall Effect sensor 3341. This can beachieved by comparing the signal to an expected range of signalscorresponding to known actuation positions as discussed above. FIG. 39illustrates the end effector 3320 in a second articulated position wherethe articulation actuator 3331 is actuated in a fully-distal position.In this configuration, the first magnet 3343 is a first distance d₂₂from the sensor 3341 and the second magnet 3345 is a second distance d₁₂from the sensor 3341. A control circuit is configured to determine theposition of the magnets 3343, 3345 by interpreting the signal from theHall Effect sensor 3341. FIG. 40 illustrates the end effector 3320 in anon-articulated position. In this configuration, the first magnet 3343is a first distance d₂₃ from the sensor 3341 and the second magnet 3345is a second distance d₁₃ from the sensor 3341. A control circuit isconfigured to determine the position of the magnets 3343, 3345 byinterpreting the signal from the Hall Effect sensor 3341.

The sensing system 3340 can be used by a control circuit to determinethe actual position of the end effector 3320 relative to the shaft 3310without having to monitor the output of the articulation drive systemmotor. In at least one instance, the control circuit is configured toautomatically adjust a motor control program configured to actuate thearticulation actuator 3311 according to a desired outcome based on themonitored position of the end effector 3320. For example, a user mayinstruct the instrument to place the end effector 3320 in anon-articulated configuration. The sensing system 3340 can be used todetermine the actual position of the end effector 3320. If the endeffector 3320 does not fully attain the desired position, the controlcircuit can be configured to alert a user and/or automatically adjustthe motor control program to actuate the articulation actuator 3311until the sensing system 3340 detects the end effector 3320 in thedesired position.

A sensing system such as the sensing system 3340, for example, thatmeasures a distal-most movable actuation component can provide a greaterdegree of accuracy compared to sensing systems that measure intermediatemovable actuation components. For example, when measuring a movableactuation component upstream of the distal-most movable actuationcomponent, the sensing system may not be able to detect any slop orbacklash in the system downstream of the intermediate component beingsensed. Measuring the distal-most movable actuation component of a drivesystem ensures that all variance in the drive system is detected and,thus, can be compensated for, for example. In at least one instance, thesecond magnet 3345 is positioned on the end effector 3320 itself.

In at least one instance, the inertia and/or friction of a kinematicsystem within a surgical instrument assembly is configured to bemonitored. In at least one instance, a control circuit is configured toadjust a motor control program corresponding to the monitored kinematicsystem. In at least one instance, adjustments can be performed tominimize excessive loading on a drive member, eliminate an impact eventof a drive member, and/or ensure complete actuation strokes of a drivemember, for example.

In at least one instance, a control circuit is configured to monitorlocal displacement and velocity of a drive member as well as motorcurrent of a motor configured to actuate the drive member. Theseparameters can be monitored during an acceleration and/or braking eventof the drive member to determine an inertia of the system. The controlcircuit can then determine if the determined inertia is different froman expected inertia. As a result, inertia detection can be used toadjust a control program of the motor to more accurately execute suchbreaking and/or acceleration events of the drive member. In at least oneinstance, a control circuit is configured to alter the initiation timingof a braking cycle of a drive member based on the determined inertia ofa previous braking cycle of the drive member.

In at least one instance, a control circuit is configured to prevent ahigh load impact event within a surgical stapling end effector based ona monitored inertia of a firing system within the surgical stapling endeffector. The control circuit can further be configured to ensure acomplete actuation cycle of the firing system even after an adjustmentto a braking cycle is made to prevent the high load impact event. In atleast one instance, retraction strokes also come with a risk of a highload impact event at a proximal end of the retraction stroke. In atleast one instance, a control circuit is also configured to preventproximal end high load impact events.

In at least one instance, a control circuit is configured to monitor abrake initiation trigger event such as, for example, at a determinedstroke location and/or at a maximum force threshold. Both events mayrequire a braking of a drive system. The control circuit is configuredto learn the brake initiation triggers and can prevent the drive systemfrom reaching the brake initiation triggers in subsequent firings of thedrive system. In at least one instance, a brake timing is sped up toavoid a brake initiation trigger. In at least one instance, the braketiming is slowed down to avoid a brake initiation trigger. In at leastone instance, a first test actuation could be performed within asurgical instrument assembly to determine inertia differences within thesurgical instrument assembly compared to a nominal inertia of thesurgical instrument assembly.

In various instances, a control circuit is provided to monitor frictionwithin a drive system and adjust a motor control program accordingly.For example, a closure member of a surgical instrument can be monitoredas the closure member clamps a jaw within an end effector. Theacceleration, velocity, and/or displacement of the closure member can bemonitored to map a closure event profile every time the closure memberis actuated. The control circuit is configured to adjust the motorcontrol program which actuates the closure member to ensure that theclosure event profile is as consistent as possible through the life ofthe closure member during every closure stroke. The closure system mayexperience parasitic loss and wear over time resulting in a variance inthe closure stroke of the system. The control circuit is configured tocompensate for this. In at least one instance, the control circuit isconfigured to adjust the closure stroke based on tissue thickness and/orcompressibility differences which can also be monitored.

FIGS. 41-43 depict a stretchable sensing fabric 3400 configured to senseone or more parameters of a surgical instrument assembly. Thestretchable sensing fabric 3400 comprises a body portion 3410 and aplurality of sensing materials position within the body portion 3410.The plurality of sensing materials comprise a plurality of sensingfibers 3420, 3430, 3440 configured to sense one or more parameters ofthe surgical instrument assembly. In at least one instance, the sensingfibers 3420, 3430, 3440 are configured to measure pressure, bendingstress, stretch, and/or shear force. The sensing fibers 3420, 3430, 3440comprise electrically conductive material. In at least one instance, thefibers 3420, 3430, 3440 are interwoven into the body portion 3410 of thestretchable sensing fabric 3400. In at least one instance, the bodyportion 3410 comprises an elastic silicone, for example. In at least oneinstance, the fibers 3420, 3430, 3440 are placed into a mold for thebody portion 3410 and the fibers 3420, 3430, 3440 are enveloped by amaterial of the body portion 3410. At any rate, the fibers 3420, 3430,3440 are configured to stretch, twist, and/or bend with the body portion3410. FIG. 42 illustrates the stretchable sensing fabric 3400 in arelaxed configuration and FIG. 43 illustrates the stretchable sensingfabric 3400 in a stretched configuration. The fibers 3420, 3430, 3440are configured to be connected to an electrical circuit such that acontrol circuit can monitor the resistance of the fibers 3420, 3430,3440 as the fibers 3420, 3430, 3440 change shape.

In at least one instance, the resistance of the fibers 3420, 3430, 3440can be amplified or suppressed by connecting the fibers 3420, 3430, 3440in parallel or in series. In at least one instance, each fiber 3420,3430, 3440 comprises a different material. In at least on instance, thematerial of each fiber 3420, 3430, 3440 is selected based on itsresistive properties. For example, when sensing a system with verylittle movement such as, for example, a closure member that may onlymove slightly through a closure stroke, a material and configuration maybe selected that comprises a wide range of resistance variance with verylittle stretch.

In at least one instance, the fibers 3420, 3430, 3440 may be interlockedby weaving the fibers 3420, 3430, 3440 together, for example, toincrease the available stretchable length of each fiber 3420, 3430,3440. In at least one instance, the stretchable sensing fabric 3400 isattached by way of an adhesive only to a structural member to be sensed.In at least one instance, the stretchable sensing fabric 3400 isattached to a fixed location within a shaft, for example, and astructural member to be sensed such that the stretchable sensing fabric3400 stretches relative to the shaft to which it is attached as thestructural member moves relative to the shaft. In at least one instance,a supplemental spring is provided to increase or decrease sensitivity ofthe stretchable sensing fabric 3400.

In at least one instance, the fibers 3420, 3430, 3440 are oriented inmultiple different directions and/or positioned in multiple differentplanes. In at least one instance, the stretchable sensing fabric 3400comprises a full-bridge strain gauge configuration. In at least oneinstance, the stretchable sensing fabric 3400 comprises a half-bridgestrain gauge configuration. In at least one instance, the stretchablesensing fabric 3400 comprises a quarter-bridge strain gaugeconfiguration.

In at least one instance, the stretchable sensing fabric 3400 is used tomonitor displacement, stress, and/or strain. Such parameters can bedetermined by a control circuit configured to interpret monitoredresistance signals from the fibers within the sensing fabric 3400.

In at least one instance, the body portion 3410 comprises materialproperties that effect how the fibers 3420, 3430, 3440 stretch. In suchan instance, the load applied to the body portion 3410 can be directlydetected by the fibers 3420, 3430, 3440. In at least one instance, thestretchable sensing fabric 3400 comprises EeonTex conductive textile. Inat least one instance, the stretchable sensing fabric 3400 comprisesSHIELDEX metallized conductive fabric.

In at least one instance, a transparent portion is provided within asurgical instrument drive system. A drive member itself may comprise thetransparent portion. In at least one instance, the transparent portionis a supplemental component integrated into the drive system. Opticallight diffraction can be used to detect a load applied to thetransparent portion by measuring the change in light within thetransparent portion owing to the change in the transmissibility and/orreflectivity changes in the material when it is loaded and unloaded.

In at least one instance, the stretchable sensing fabric 3400 can beused in conjunction with any movable drive members within a surgicalinstrument system. FIGS. 44 and 45 depict a surgical instrument assembly3500 comprising a surgical stapling drive member 3510 configured for usewith a surgical stapling instrument and a plurality of stretchablesensing fabrics 3400 positioned on the surgical stapling drive member3510. The surgical stapling drive member 3510 comprises a plurality ofbands 3511 stacked together and coupled to a firing member 3520configured to cut tissue and deploy staples during a staple-firingstroke. As the bands 3511 are displaced around an articulation joint,the bands 3511 bend around the articulation joint and splay relative toeach other. This bending can be detected by the stretchable sensingfabrics 3400 and can be correlated by the control system to the degreein which the end effector is articulated.

The stretchable sensing fabrics 3400 are positioned on the top 3517 ofeach band 3511. In at least one instance, the stretchable sensingfabrics 3400 are attached to each band 3511 with an adhesive, forexample. In at least one instance, the attachment means for thestretchable sensing fabrics 3400 to each band 3511 does not affect theconductive fibers within the stretchable sensing fabrics 3400. Thesurgical instrument assembly 3500 further comprises electrical contacts3531 configured to be coupled to the fabrics 3400 such that anelectrical connection can be made with a flex circuit, for example. Eachband 3511 further comprises a proximal engagement feature 3513comprising a window 3514 configured to receive a firing drive system toactuate the surgical stapling drive member 3510. The fabrics 3400 caneach stretch relative to each other to monitor one or more parameters ofeach band 3511 separately. Such a configuration can be used to monitorvarious parameters of articulation of an end effector. Such aconfiguration can also be used to detect a load applied to the firingmember 3520 as the firing member 3520 is advanced through thestaple-firing stroke.

FIGS. 46 and 47 depict a surgical instrument assembly 3600 comprisingthe shaft 3310, end effector 3320, and articulation joint 3330 of FIGS.38-40 and a sensing system 3620 configured to detect a parameter of thearticulation actuator 3311. The surgical instrument assembly 3600further comprises a firing actuator 3610 comprising a flexible memberconfigured to extend through the articulation joint 3330 and into theend effector 3320 to actuate a function of the end effector 3320 such asclosing the end effector 3320 and/or performing a staple firing stroke,for example.

The sensing system 3620 comprises a flex circuit 3630, a non-stretchableprinted circuit board 3640 coupled to the flex circuit 3630, and astretchable sensing fabric 3650 coupled to the printed circuit board3640. The flex circuit 3630 extends through the shaft 3310 and can beconnected to a surgical control interface such as a handle and/or asurgical robot, for example. The printed circuit board 3640 is attachedto the articulation actuator 3311 and moves with the articulationactuator 3311. In certain instances, the printed circuit board 3640 isattached to a fixed location such as the shaft 3310, for example. Thestretchable sensing fabric 3650 comprises electrical circuits which areconnected to electrical contacts on the printed circuit board 3640 and,likewise, the flex circuit 3630 comprises electrical circuits which areconnected to another set of contacts on the printed circuit board 3640.As a result, signals can be transmitted between the sensing fabric 3650,the printed circuit board 3640, the flex circuit 3630, and the surgicalcontrol interface.

The stretchable sensing fabric 3650 is configured to stretch as the endeffector 3320 is articulated by the articulation actuator 3311. Morespecifically, a distal end of the stretchable fabric 3650 is attachedthe second articulation link 3333 such that as the end effector 3320 isarticulated, the stretchable sensing fabric 3650 stretches. As thestretchable sensing fabric 3650 changes shape when it stretches, theconductive fibers within the stretchable sensing fabric 3650 also changeshape and generate a change in resistance, for example. This change inresistance of the conductive fibers within the stretchable sensingfabric 3650 can be detected by a control circuit to determine aparameter, such as the orientation and/or position, of the articulationactuator 3311, articulation joint 3320, and/or end effector 3320. Invarious instances, the control circuit is in the printed circuit board3640 and/or the surgical control interface.

In at least one instance, the stretchable sensing fabric 3650 is used todetermine the exact position of the articulation actuator based onpre-determined known stretch characteristics of the stretchable sensingfabric 3650. In at least one instance, the stretchable sensing fabric3650 is used to determine the degree of articulation of the end effector3320 relative to the shaft 3310. In at least one instance, thestretchable sensing fabric 3650 is used to determine the speed and/oracceleration of the articulation actuator 3311. In at least oneinstance, the stretchable sensing fabric 3650 is used to directlymeasure one or more rotational characteristics of the articulation link3333 such as, rotational velocity and/or rotational displacement, forexample.

FIG. 47 depicts the sensing system 3620 where the non-stretchableprinted circuit board 3640 is fixed relative to the shaft 3310. Thestretchable sensing fabric 3650 comprises a first stretchable portion3651 and a second stretchable portion 3653. In at least one instance, aportion of the stretchable sensing fabric 3650 is fixed to thearticulation actuator 3311 in between the first stretchable portion 3651and the second stretchable portion 3653. In such an instance, multipleregions of stretching can be sensed and can each be used to determineone or more parameters of the surgical instrument assembly 3600. As canbe seen in FIG. 47, multiple positions of the second articulation link3333 are illustrated showing different stretch lengths of the secondstretchable portion 3653 when in each position. These different lengthscan comprise different corresponding resistance profiles of conductivefibers within the stretchable sensing fabric 3650. These differentcorresponding resistance profiles can be assessed by a control circuitas described herein. The control circuit can then determine one or moreparameters such as the degree of rotation, and/or end effector position,for example, based on the resistance profile detected.

FIGS. 48 and 49 depict graphs 3701, 3703 in connection with a controlcircuit for use with a surgical instrument assembly configured todetermine a load profile and adjust an operational control program ofthe surgical instrument assembly based on the determined load profile.The graph 3701 illustrates multiple different load profiles within atissue cutting knife that, in at least one instance, define anacceptable range of loads for the tissue cutting knife. By way ofanother example, the acceptable range of load profiles is illustrated inthe graph 3703 relative to an actual load profile 3704 detected by thecontrol circuit using any suitable sensing system such as thosedisclosed herein. As can be seen in the example of FIG. 49, the actualload profile 3704 detected is above the range of acceptable loadprofiles. The control circuit can then take action accordingly. In atleast one instance, the control circuit is configured to automaticallyadjust a control program of the surgical instrument assembly to reducethe load profile such as slow down a drive member and/or pause theactuation of the drive member, for example. In certain instances, thecontrol circuit is configured to reduce the maximum current available tothe electric motor to reduce the load profile. In certain instances, thecontrol system can modify the time, or pause, between operational stepswhen a discrepancy is detected. In at least one instance, the controlsystem can increase the pause between clamping the end effector andperforming a staple firing stroke, for example. In at least oneinstance, the control circuit is configured to alert a user that theload profile is outside of the acceptable range and request input from auser how to proceed. In at least one instance, the control circuit isconfigured to lock out the staple firing drive system upon detecting aload profile outside the range of acceptable load profiles. In suchinstances, other drive systems can be operated to retract the staplefiring drive, open the end effector, and/or straighten the end effector,for example.

In at least one instance, the control circuit is configured to determinea tissue thickness within an end effector and define the range ofacceptable load profiles based on the determined tissue thickness. If ameasured load profile is outside the defined range of acceptable loadprofiles, a user may be alerted that an irregularity has occurred duringan actuation stroke. For example, a foreign object, such as a surgicalclip, for example, may be present within the end effector causing theload profile to exceed the defined range of acceptable load profilesbased on the determined tissue thickness.

In at least one instance, load profiles are monitored over time andadjustments can be made and/or recommended, for example, by a controlcircuit based on multiple actuations of the surgical instrumentassembly. The control circuit may determine a steadily increasing loadprofile during each subsequent actuation of the surgical instrumentassembly and may alert a user of the increasing load profiles. In atleast one such instance, multiple load profiles must be measured andevaluated prior to action being taken by a control circuit. In at leastone instance, the force required to drive an end effector function witha worn component may increase over time. In such an instance, a user maybe directed to swap out the surgical instrument assembly for a differentone based on the detected wear. In at least one instance, the controlcircuit is configured to adjust a motor control program to compensatefor the worn component to use up any remaining life of the worncomponent. For example, once a certain threshold of wear is detected, acontrol circuit can use a pre-determined use profile to determine thatthe surgical instrument assembly may be actuated a maximum of five moretimes before locking the surgical instrument assembly, for example, outand/or taking another action.

Further to the above, the load profiles of a surgical stapling assemblycan be measured and monitored over time, i.e., throughout the life ofthe surgical stapling assembly. In various instances, a surgicalstapling attachment assembly is configured to use replaceable staplecartridges and, after each firing of a replaceable staple cartridge, aload profile can be logged into the memory of the surgical instrumentcontrol system. In at least instance, adjustments to the operationalcharacteristics of the surgical stapling attachment assembly can be madefor each subsequent replaceable staple cartridge installed within thesurgical stapling attachment assembly. In at least one instance, acontrol circuit can determine batch-specific load characteristics of abatch of staple cartridges. In such an instance, a batch-specificcontrol program can be created and implemented by the control circuitbased on the load profiles measured when using staple cartridges fromthe batch of staple cartridges. In at least one instance, a controlcircuit is configured to utilize manufacturing data communicated to thecontrol circuit by the staple cartridge itself using an RFID chip, forexample. In such an instance, the control circuit can log each eventwith matching manufacturing data in a grouping of firings to determine asuitable control program for staple cartridges with matchingmanufacturing data. Matching manufacturing data may include, forexample, the same serial number, similar serial numbers, and/or serialnumbers within a range of serial numbers, for example.

In various instances, a surgical instrument comprises a shaft, an endeffector, and one or more drive systems configured to actuate the shaftand/or the end effector. The end effector comprises a first jaw and asecond jaw which is rotatable relative to the first jaw between an open,unclamped position and a closed, clamped position. One of the drivesystems comprises a jaw closure system configured to close the secondjaw. The surgical instrument can further comprise an articulation jointrotatably connecting the end effector to the shaft and an articulationdrive system configured to articulate the end effector relative to theshaft. The surgical instrument can also comprise a tissue cutting knifewhich is movable distally during a firing stroke and a knife drivesystem configured to drive the tissue cutting knife distally and retractthe tissue cutting knife proximally. The surgical instrument furthercomprises a housing, such as a handle, for example, which rotatablysupports the shaft such that the shaft is rotatable about a longitudinalaxis relative to the housing. The surgical instrument can furthercomprise a drive system configured to rotate said shaft in clockwise andcounter-clockwise directions about the longitudinal axis.

Each of the drive systems of the surgical instrument discussed above aredriven by an electric motor. In various instances, each of the drivesystems comprises its own electric motor which are separately andindependently controlled by a controller, or control circuit. In otherinstances, at least two or more of the drive systems are driven by asingle electric motor which is controlled by the controller. In suchinstances, the surgical instrument comprises a shifter, or transmission,which allows the electric motor to separately and independently drivedifferent drive systems. In any event, the controller is responsive touser inputs, sensor inputs from within the surgical instrument, and/orsensor inputs external to the surgical instrument. In various instances,the controller comprises a control system including a processor and amemory device in the housing, a processor and a memory device in theshaft, and/or a wiring harness connecting and/or communicating with thevarious components of the control system, including the sensors, forexample. In at least one instance, the control system comprises a flexcircuit extending within the shaft that is in communication with acontrol system processor, such as a microprocessor, for example. Theflex circuit can comprise a flexible substrate that is flexible enoughto extend between the shaft and the end effector and accommodate thearticulation of the end effector, discussed above, and electrical tracesdefined on and/or contained within the flexible substrate.

In at least one instance, further to the above, the flex circuitcomprises a plurality of polyimide layers and metallic circuitspositioned intermediate the polyimide layers. In at least one instance,the metallic circuits comprise copper frames while, in some instances,the metallic circuits are comprises of conductive ink, for example.Certain circuits within the flex circuit are wider, thicker, and/or havea higher conductivity than others and may be more suitable forconducting electrical power loads, whereas certain circuits that arenarrower, thinner, and/or have a lower conductivity may be more suitablefor conducting data communication signals, for example. In variousinstances, the power loads can create magnetic and/or electrical fieldswhich can interfere with the data communication signals and, as aresult, the power circuits can be separated and/or segregated from thecommunication circuits. In at least one instance, the power circuits arearranged in a power backbone within the flex circuit while thecommunication circuits are arranged in a communication backbone withinthe flex circuit. In various instances, the power backbone comprises afirst segment within the flex circuit while the communication backbonecomprises a second segment within the flex circuit. In at least oneinstance, the second, or communication segment, can be furthersub-segmented. Whether or not a segment could be referred to as asub-segment, they can be referred to as a segment and will be for thesake of convenience herein.

In various instances, further to the above, a flex circuit comprises aplurality of segments which are in communication with the controller. Inat least one instance, the segments comprise sensor segments. Forinstance, a flex circuit can comprise a first segment including a firstsensor, a second segment including a second sensor, and a third segmentincluding a third sensor. The first sensor is configured to detect, at afirst location, the status of a component of the surgical instrument,the second sensor is configured to detect, at a second location, thestatus of a component of the surgical instrument, and the third sensoris configured to detect, at a third location, the status of a componentof the surgical instrument. That said, a flex circuit can comprise anysuitable number of sensors and sensor circuit segments. In variousinstances, each sensor circuit segment is configured to evaluate thestatus of a different component while, in other instances, two or moresensor circuit segments can be used to evaluate the same component.Referring to FIGS. 51 and 52, a surgical instrument assembly 3000comprises a staple cartridge 3020 and a firing member 3010 that is movedfrom a proximal end 3025 of the staple cartridge 3020 to a distal end3027 of the staple cartridge 3020 during a firing stroke. In variousinstances, the firing member 3010 comprises one or more ramped surfacesconfigured to eject staples from the staple cartridge 3020 while, insome instances, the firing member 3010 comprises a tissue cutting edge.In any event, a magnet 3031 is mounted to the firing member 3010 whichis tracked by a sensing system 3030 including a proximal sensor 3033positioned at the proximal end 3025 of the staple cartridge and a distalsensor 3035 positioned at the distal end 3027. The magnet 3031 comprisesany suitable magnetic element including one or more magnetic poles andcan be comprised of iron and/or nickel, for example. The sensors 3033and 3035 comprise Hall Effect sensors, for example, but could compriseany suitable type of sensor. Referring to graph 4120 in FIG. 52, theproximal sensor 3033 generates a magnetic field which is distorted oraffected by the magnet 3031 when the firing member 3010 is in itsproximal position. As the firing member 3010 is advanced distally duringits firing stroke, the magnet 3031 moves away from the proximal sensor3033 and, as a result, the effect that the magnet 3031 has on themagnetic field produced by the proximal sensor 3033 diminishes. Thischange in the magnetic field is detected by the controller which thecontroller interprets as the firing stroke being initiated. Similarly,referring to graph 4130 in FIG. 52, the magnet 3031 begins to distortand effect a magnetic field produced by the distal sensor 3035 as thefiring member 3010 is moved distally during the firing stroke which isalso detected by the controller which interprets this distortion as thefiring stroke being completed.

The proximal sensor 3033 is part of a proximal sensor flex circuitsegment and the distal sensor 3035 is part of a distal sensor flexcircuit segment. The proximal sensor segment and the distal sensorsegment are in communication with a control circuit defined on the flexcircuit. In various instances, the control circuit comprises a microchipmounted to the flex circuit, for example. The proximal sensor 3033 isconfigured to provide or transmit data to the control circuit via theproximal sensor segment and the distal sensor 3035 is configured toprovide or transmit data to the control circuit via the distal sensorcircuit. Further to the above, in various instances, the proximal sensor3033 produces and detects a magnetic field. The presence of the magnet3031 distorts the magnetic field and the proximal sensor 3033 producesan analog signal, the voltage of which is proportional in magnitude withthe detected magnetic field. The distal sensor 3035 works the same way.In such instances, as a result, the control circuit receives constantanalog data streams from the proximal sensor 3033 and the distal sensor3035. In various instances, the microchip of the control circuit can beconfigured to intermittently sample the data streams provided by thesensors 3033 and 3035. Alternatively, the proximal sensor 3033 and/orthe distal sensor 3035 can comprise a digital Hall Effect sensor. Ineither event, the controller microchip can comprise an input dedicatedto each sensor segment. In various instances, the control circuit cancomprise a multiplexer, or MUX, that is configured to receive aplurality of data streams and merge the data streams into a signaloutput signal, for example. In any event, the control circuit utilizesthe data received from the sensors to alter the operation of thesurgical instrument, as described in greater detail below.

As discussed above, the surgical instrument comprises a proximal sensorcircuit for detecting the movement of the firing member 3010 at thebeginning of the staple firing stroke and a distal sensor circuit fordetecting the movement of the firing member 3010 at the end of thestaple firing stroke. In at least one embodiment, the control circuitactively monitors the proximal sensor circuit and distal sensor circuitthroughout the staple firing stroke. Similarly, in at least oneembodiment, the control circuit actively monitors the proximal sensorcircuit and the distal sensor circuit throughout the retraction strokeof the firing member 3010. Thus, the control circuit requires anoverall, or total, data bandwidth which can accommodate a first databandwidth consumed by the proximal sensor segment and a second databandwidth consumed by the distal sensor segment. Moreover, in suchinstances, the control circuit requires a power source sufficient topower the proximal sensor segment and the distal sensor segment at thesame time. In various instances, however, it may be desirable for alarger portion of the total available bandwidth and/or power to bededicated to one sensor segment than another at a given time. Forinstance, the control circuit can be configured to devote a larger databandwidth and power to the proximal sensor segment than the distalsensor segment at the beginning of the staple firing stroke and, then,devote a larger data bandwidth and power to the distal sensor segmentthan the proximal sensor segment at the end of the staple firing stroke.In such instances, the control circuit can focus its sensing capacity towhere the firing member 3010 is located. Such an arrangement can behighly suited for actively monitoring the initial acceleration of thefiring member 3010 and the deceleration of the firing member 3010 at theend of the staple firing stroke. Stated another way, devoting an equalshare of data bandwidth to the distal sensor segment at the initiationof the staple firing stroke is not an efficient use of the databandwidth of the control circuit as the distal sensor segment does notmonitor the firing member 3010 at the beginning of the staple firingstroke or the distal sensor segment is not as accurate as the proximalsensor segment in such instances. Similarly, devoting an equal share ofdata bandwidth to the proximal sensor segment at the end of the staplefiring stroke is not an efficient use of the data bandwidth of thecontrol circuit as the proximal sensor segment does not monitor thefiring member 3010 at the end of the staple firing stroke or theproximal sensor segment is not as accurate as the distal sensor segmentin such instances.

In various embodiments, the control circuit can be configured toselectively power and de-power the sensor segments of the flex circuit.In at least one such embodiment, the control circuit can apply asufficient voltage to the proximal sensor segment to power the proximalHall Effect sensor 3033 at the outset of the staple firing stroke suchthat the proximal sensor 3033 can sufficiently emit and detect itsmagnetic field, as discussed above, and, at the same time, not apply asufficient voltage to the distal sensor segment to sufficiently powerthe distal Hall Effect sensor 3035. In such instances, the databandwidth devoted to the distal sensor segment can be minimize oreliminated such that the control circuit can focus its bandwidth of theproximal sensor segment. Stated another way, the control circuit canplace the distal sensor segment in a sleep mode at the beginning of thestaple firing stroke. As the firing member 3010 is advanced distally,however, the control circuit can wake up the distal sensor segment byapplying a sufficient voltage to the distal sensor segment and dedicatea sufficient portion of its data bandwidth to the distal sensor segment.Moreover, the control circuit can then place the proximal sensor segmentin a sleep mode while the control circuit focuses its data bandwidth onthe distal sensor segment. Such an arrangement can allow the controlcircuit to accurately brake, or slow down, the firing member 3010 at theproper time and/or stroke length, for example.

The teachings of the above-discussed examples could be used in anysuitable systems in the surgical instrument. For instance, such anarrangement could be used in connection with articulation systemscomprising a first sensor for detecting the articulation of the endeffector in a first direction and a second sensor for detecting thearticulation of the end effector in a second direction. Also, forinstance, such an arrangement could be used in connection with theclosure drive system. Moreover, such arrangements could be adapted foruse with rotatable drive members.

In various embodiments, further to the above, the control circuit can beconfigured to intermittently ask the sensor segments to provide data.For instance, the sensors can be in a sleep mode in which they are notactively supplying voltage signals above a threshold, such as a noisethreshold, to the control circuit until the control circuit selectivelysupplies a ping, or wake, signal to one or more of the sensor segmentsand, in such instances, the activated sensor segment, or segments, cansupply a voltage signal to the control circuit above the noisethreshold. In at least one embodiment, each sensor segment comprises aprocessor and a signal transmitter in communication with the sensorwhich are activated by an ask signal from the control circuit. In suchembodiments, the each sensor segment is configured to provide at leastsome pre-processing of the data before it is transmitted to the controlcircuit. In at least one instance, the segment processor is configuredto convert an analog signal to a digital signal and then transmit thedigital signal to the control circuit. In various instances, the segmentprocessor is configured to modulate the byte size of the datatransmitted to the control circuit from the sensor segment. Forinstance, when the control circuit powers a sensor segment with avoltage magnitude within a first range, the sensor segment supplies datato the control circuit having a first byte size and, when the controlcircuit powers the sensor segment with a voltage magnitude within asecond range that is different than the first range, the sensor segmentsuppliers data to the control circuit having a second byte size which isdifferent than the first byte size. In at least one instance, the sensorsegment processor supplies data with smaller byte sizes when the voltagemagnitude is smaller and supplies data with larger byte sizes when thevoltage magnitude is larger. In such instances, the sensor segmentprocessor is configured to interpret the receipt of lower voltagemagnitudes as an instruction to operate in a low-power/low-bandwidthmode and the receipt of higher voltage magnitudes as an instruction tooperate in a high-power/high-bandwidth mode. Any suitable arrangementcould be used.

In various embodiments, further to the above, the control circuit isconfigured to issue instructions to the sensor segments to provide dataat a certain bandwidth. In at least one embodiment, the control circuitis configured to compare the total data bandwidth to the data bandwidththat is currently being consumed and issue instructions to the sensorsegments to provide their data at bandwidths that will not overload, orexceed, the remaining available bandwidth. As more and/or less availabledata bandwidth is available, the control circuit can modify itsinstructions to the sensor segments. In at least one instance, eachsensor segment comprises a signal receiver configured to receive asignal from the control circuit that includes data, or a plurality ofinstructions, for delivering the sensor data to the control circuit atthe desired voltage magnitude, bandwidth, and/or byte size, for example.When the sensor segment receives a first set of instructions, the sensorsegment delivers the sensor data in a first format and, when the sensorsegment receives a second set of instructions, the sensor segmentdelivers the sensor data in a second format.

In various instances, further to the above, the control circuit canactivate a sensor when a drive component has reached a specific positionin its motion. For example, the control circuit can activate the distalsensor segment when the firing member 3010 reaches a position which is 5mm from the end of the staple firing stroke. In at least one suchinstance, the distal sensor segment does not transmit data to thecontrol circuit until the distal sensor segment is activated when thefiring member 3010 reaches the 5 mm remaining position and, at suchpoint, the distal sensor segment transmits data to the control circuitat a high bandwidth. To achieve this, the control circuit monitors thetravel of the firing member 3010 during the firing stroke. In at leastone instance, the control circuit uses the data from the proximal sensorsegment to assess the position of the firing member 3010; however, thefiring member 3010 is no longer adjacent the proximal sensor 3033 andthe accuracy of the data from the proximal sensor 3033 may not bereliable enough to rely on. As such, the control circuit can compriseone or more sensor systems which can more measure the travel of thefiring member 3010 more reliably. For instance, the control circuit cancomprise a sensor system which monitors another drive component of thestaple firing system such as the output shaft of the electric motor ofthe staple firing drive and/or a translatable shaft driven by theelectric motor, for example. Various other arrangements are described ingreater detail below.

In various embodiments, further to the above, a surgical instrumentcomprises a wiring harness, such as a flex circuit, for example, whichcomprises one or more integrated sensors that are positioned andarranged to measure the motion of a component locally, i.e., at alocation adjacent to the component being monitored. In variousinstances, as discussed above, the component is rotatable. In at leastone such instance, an array of magnetic elements are mounted, attached,and/or integrated to the rotatable component which produce magneticfields that are detected by an array of coil sensors mounted in theshaft of the surgical instrument. The magnetic elements are arranged ina circular pattern and the coil sensors are arranged in a circularpattern that matches the circular pattern of the magnetic elements suchthat the magnetic fields produced by the coil sensors are affected bythe magnetic fields produced by the magnetic elements. Each of themagnetic elements comprises at least one negative pole and at least onepositive pole and the magnetic elements are arranged in an alternatingmanner such that the positive pole of a first magnetic element facesproximally and the adjacent magnetic elements are arranged such that thetheir negative poles are facing proximally, and so forth. Alternatively,the rotatable component comprises two magnetic elements mounted to acylindrical body—a first magnetic element positioned on a first side ofthe cylindrical body and a second magnetic element positioned on asecond, or opposite, side of the cylindrical body, i.e., the twomagnetic elements are positioned 180 degrees apart. In this embodiment,the flex circuit comprises a coil sensor which is mounted tosequentially detect the first magnetic element and the second magneticelement in an alternating manner. The positive pole of the firstmagnetic element generally faces the coil sensor while the negative poleof the second magnetic element generally faces the coil sensor such thatthe sensing system has a resolution for each half rotation of thecylindrical body. A higher degree of resolution can be achieved withmore magnetic elements and/or more coil sensors.

In various embodiments, further to the above, a surgical instrumentcomprises a wiring harness, such as a flex circuit, for example, whichcomprises one or more integrated sensors that are positioned andarranged to measure the motion of a component locally, i.e., at alocation adjacent to the component being monitored. In variousinstances, as discussed above, the component is translatable. In atleast one such instance, the flex circuit comprises a Hall Effect sensorand the translatable component comprises a magnetic element mountedthereto. During use, the translatable component is moved through a fullrange of motion between a first position and a second position. The HallEffect sensor emits a magnetic field that is co-extensive with the fullrange of motion of the magnetic element such that the Hall Effect sensorcan monitor the component throughout its entire range of motion.

In various embodiments, further to the above, the flex circuit comprisesa first Hall effect sensor and a second Hall effect sensor and thetranslatable component comprises a first magnetic element and a secondmagnetic element. In at least one embodiment, the second Hall Effectsensor is positioned distally, or longitudinally, relative to the firstHall Effect sensor. Similarly, the second magnetic element is positioneddistally, or longitudinally, relative to the first magnetic element. Inuse, the translatable component is moved distally from a proximal,unfired position to a distal, fired position during a firing stroke.During the initial motion of the translatable component, the firstmagnetic element is detectable by the first Hall Effect sensor but notthe second Hall Effect sensor and, moreover, the second magnetic elementis not detectable by either the first Hall Effect sensor or the secondHall Effect sensor. As the first magnetic element moves out of the rangeof the first Hall Effect sensor during the firing stroke, the secondmagnetic element moves into range of the second Hall Effect sensor.Notably, the first magnetic element does not enter into the range of thesecond Hall Effect sensor in this embodiment. As such, the entire rangeof motion of the translatable component can be monitored, collectively,by the first and second Hall Effect sensors. In at least one instance,there is a small amount of overlap during the firing stroke in which thefirst Hall Effect sensor can detect the first magnetic element and thesecond Hall Effect sensor can detect the second magnetic element. Inother embodiments, there is no such overlap and the monitoring of thefirst and second Hall Effect sensors is line-to-line. Theabove-described arrangements would be useful to a low stroke actuationlike an energy device or grasper/dissector (0.250″ total stroke, forexample) where the resolution of the stroke is highly correlated to achange in tissue clamp load for a small increment in stroke locationchange. The jaw actuator of a 5 mm grasper/dissector is typicallybetween 0.1″-0.3″ with +−0.05″, for example, equating to several poundsdifference in jaw tissue compression once closed onto tissue.

A surgical instrument 4000 comprising a clamping jaw described above isillustrated in FIG. 50. The surgical instrument 4000 comprises a shaft4010 and an end effector 4030. The end effector 4030 comprises anon-translating blade 4031 configured to apply vibratory energy to thetissue of a patient and, in addition, a clamp jaw 4033 rotatable betweenan open position and a closed position by a closure driver 4020. Theclamp jaw 4033 is rotatably pinned to the shaft 4010 such that the clampjaw 4033 rotates about a fixed axis and the closure driver 4020 ispinned to the clamp jaw 4033 such that, when the closure driver 4020 ispulled proximally, the closure driver 4020 rotates the clamp jaw 4033toward the stationary jaw 4031. Correspondingly, the closure driver 4020is moved distally to drive the clamp jaw 4033 toward its open position.The surgical instrument 4000 further comprises a sensing system 4040configured to detect the movement of the closure driver 4020 and, thus,the movement of the clamp jaw 4033. The sensing system 4040 comprises afirst, or proximal, magnetic element 4043 mounted to the closure driver4020, a second, or distal, magnetic element 4045 mounted to the closuredriver 4020, and a sensor 4047 mounted to the shaft 4010 configured todetect the motion of the magnetic elements 4043 and 4045. Notably, thefirst magnetic element 4043 comprises a negative pole which generallyfaces the sensor 4047 and the second magnetic element 4045 comprises apositive pole which generally faces the sensor 4047.

Further to the above, the sensing system 4040 comprises a controller incommunication with the sensor 4047 configured to interpret the output ofthe sensor 4047 to assess the position of the closure driver 4020. Owingto the opposite polarities of the first magnetic element 4043 and thesecond magnetic element 4045, the motion of the closure driver 4020 hasa high degree of resolution. In various instances, the sensor 4047 andthe controller co-operate to detect the arrival and departure of themagnetic elements 4043 and 4045 within its magnetic field and, with thisdata, determine the orientation of the clamp jaw 4033. For a first givenvalue of the sensor 4047 reading, the sensing system 4040 can determinethat the clamp jaw 4033 is in a fully-open position (a). For a secondgiven value of the sensor 4047 reading, the sensing system 4040 candetermine that the clamp jaw 4033 is in a partially-closed position (b).For a third given value of the sensor 4047 reading, the sensing system4040 can determine that the clamp jaw 4033 is in a closed position (c)in which the clamp jaw 4033 applies a low pressure to the tissuecaptured between the jaws 4031 and 4033, and for a fourth given value ofthe sensor 4047 reading, the sensing system 4040 can determine that theclamp jaw 4033 is applying a high pressure to the tissue in position(c1).

In various embodiments, a sensing system of a surgical instrumentcomprises a plurality of capacitive plates, such as a first capacitiveplate and a second capacitive plate, for example. As a translatablecomponent passes over the capacitive plates, the sensing system is ableto detect capacitance changes in the capacitive plates. In variousinstances, the first and second capacitive plates are arranged inparallel. In certain instances, the translatable component passes overthe first capacitive plate and the second capacitive plate. With thisinformation the control circuit is able to assess the position, speed,and/or direction of the translatable component.

In various embodiments, a sensing system of a surgical instrumentcomprises one or more optical sensors that are used to track the motionof a component. In at least one embodiment, the flex circuit comprisesan optical sensor and the component comprises a light emitting diode, orother light source. When the component is advanced through its firingstroke, the intensity of light emitted from the LED changes as the LEDapproaches the optical sensor and/or as the LED moves away from theoptical sensor. With the data from the optical sensor, the controlcircuit of the surgical instrument can determine the position, speed,and/or direction of the movable component. In various other embodiments,both the LED and the optical sensor can be mounted to flex circuit inthe surgical instrument. In such embodiments, the movable componentscomprises through holes defined therein which, when aligned with theLED, allow the light emitted by the LED to be detected by the opticalsensor. In at least one instance, the control circuit counts the pulsesof light to assess the position, speed, and/or direction of the movablecomponent. The control circuit is also able to assess partial pulses oflight owing to partial alignment of an aperture with the LED and theoptical sensor. In at least one instance, a partial obscurement of thelight may be calculated to further refine the detection of the positionof the movable member.

In various instances, robotic surgical systems are configured to be usedwith many different surgical instrument attachments. In such instances,the different surgical instrument attachments can each comprise sensingsystems comprising sensors and corresponding triggers and actuatorsconfigured to be sensed by the sensing systems. In at least oneinstance, triggers of a first surgical attachment may interfere withsensor readings of a second surgical attachment. For example, the firstsurgical attachment and the second surgical attachment may each comprisea sensing system including a Hall Effect sensor and/or a magnetic systemwhich can effect or interfere with one another. When the surgicalinstrument attachments come in proximity to each other to an extentwhere the magnet of the first surgical instrument attachments interfereswith the Hall Effect sensor of the second surgical instrumentattachment, for example, the control system can utilize an interferenceresolution system to properly operate the surgical instrumentattachments, as described below.

Further to the above, a control circuit is provided to determine whenHall Effect sensor readings of the attached surgical instrumentattachment are caused and/or affected by a magnet or magnetic sourceexternal to the intended trigger of the attached surgical instrumentattachment. In at least one instance, a range of Hall Effect sensorvalues can be stored in a memory and correspond to expected values ofthe attached surgical instrument attachment. Should the control circuitsee any values outside the specified range, the control circuit wouldthen conclude that the sensing system within the attached surgicalinstrument attachment is being interfered with. In at least oneinstance, if signals are being received by the control circuit that donot correspond to an expected signal based on a monitored parameter of amotor driving an actuator of the attached surgical instrumentattachment, the control circuit would then conclude that the sensingsystem within the attached surgical instrument attachment is beinginterfered with. Also, for example, if the Hall Effect sensor signal isfluctuating and a motor encoder monitoring movement of the motor isdetecting no motor movement, then the control circuit would concludethat the sensing system of the attached surgical instrument attachmentis being interfered with.

In at least one instance, sensors are provided within the shaft of amodular attachment to specifically sense external interference. Forexample, a Hall Effect sensor may be provided within the shaft of theattached surgical instrument attachment to sense external magnets thatmay be positioned in surgical instruments in close proximity to theattached surgical instrument attachment. A control circuit can monitorthe Hall Effect sensor to determine if a nearby surgical instrumentattachment comprising a magnet is in close proximity to the attachedsurgical instrument attachment.

In at least one instance, the control circuit is configured to takeaction within the surgical system if outside interference is detected.In at least one instance, the control circuit is configured to disablethe sensing system local to the attached surgical instrument attachmentso that any interference with the sensing system does not affect theoperation of the attached surgical instrument attachment. In at leastone instance, the control circuit is configured to ignore theinterference based on its magnitude. For example, the interference maybe below a certain threshold that may not affect the local sensingsystem. In such an instance, the local sensing system is used and thecontrol circuit continues to monitor for possible increases ininterference. In at least one instance, if the interference isdetermined to be a constant magnitude, the expected range of the sensorsin the sensing system can be adjusted to compensate for the constantmagnitude interference thereby allowing the local sensing system tocontinue to be used. In at least one instance, a constant magnitude ofinterference can be subtractively eliminated such that the constantmagnitude of interference does not affect the local sensing system.

In at least one instance, a plurality of sensors are configured to beused to detect outside interference. In such an instance, the locationof the interference can be determined by triangulating the interferencesignals. In such an instance, the interference can be identified andremoved by a user and/or the surgical robot.

In at least one instance, multiple sensing systems within the attachedsurgical instrument attachment can be configured to trigger and sensoreach other. Such local interference can be predictable and utilized asan asset in sensing one or more parameters of one or more actuatorswithin the attached surgical instrument attachment. For example, asurgical stapling attachment comprises an actuator configured to clampan end effector as well as eject staples from the end effector. In suchan instance, one sensing system comprising a magnet and a Hall Effectsensor is positioned within the closure stroke and a second sensingsystem comprising a magnet and a Hall Effect sensor is positioned withinthe firing stroke. In such a system, the Hall Effect sensor within theclosure stroke may be affected by the magnet of the sensing system. Thisoverlap can be predictable and can provide more accurate detection of aparameter of the actuator during both the closure stroke and the firingstroke.

In at least one instance, sensors of a sensing system local to anattached surgical instrument attachment affected by outside interferencecan be temporarily switched to another sensing system if the parametersensed by the sensing system is important for proper operation of theattached surgical instrument attachment. For example, if the Hall Effectsensor of a sensing system is effected by outside interference, acontrol circuit may switch to a different monitoring sensing systemalready equipped within the surgical instrument attachment. In at leastone such instance, the control system can shift from monitoring aposition sensor in the shaft to a motor position sensor.

In at least one instance, outside interference to a local sensing systemmay not be able to be adjusted or compensated for. In such an instance,action may be taken by a control circuit. In at least one instance, analert may be sent to the robotic surgical system and/or the user. In atleast one instance, the surgical instrument attachment may be locked outsuch that, until the local sensing system re-assumes an operable state,the surgical instrument attachment is locked out by the control circuit.In at least one instance, the control circuit can place the surgicalinstrument attachment into a limp mode activating a low-power actuationstate, for example. When the control system determines that it is beinginterfered with, in various instances, the control system can slow thespeed of the drive system, reduce the acceleration of the drive system,and/or reduce the maximum current that can be drawn by the electricmotor, for example. In certain instances, the control system can modifythe time, or pause, between operational steps when a discrepancy isdetected. In at least one instance, the control system can increase thepause between clamping the end effector and performing a staple firingstroke, for example.

FIG. 53 depicts a surgical instrument system 6000 comprising a roboticsurgical interface 6010 and a plurality of surgical instrumentattachments 6020 configured to be attached to the robotic surgicalinterface. The surgical instrument system 6000 comprises a wirelesscommunication network. The surgical instrument attachments 6020 areconfigured to communicate with each other prior to any of the surgicalinstrument attachments 6020 being attached to the robotic surgicalinterface 6010. The surgical instrument attachments 6020 can communicatethe status of each attachment 6020, for example, to each otherindicating which surgical instrument attachment 6020 is ready to beattached to the robotic surgical interface 6010. Such information may beprovided by the attachment itself and its current state and/or may beprovided by a hub based on which attachment has already been indicatedby the hub to be attached to the robotic surgical interface 6010. In atleast one instance, color coded lights can be used on the surgicalinstrument attachments to indicate various things. For example, theattachments 6020 can communicate each other's status such that theattachments 6020 can identify and direct which attachment 6020 is to beattached to the robotic surgical interface 6010 for a given surgicalprocedure.

In various instances, the attachments 6020 can communicate with oneanother to communicate their proximity to one another. In suchinstances, a first attachment 6020 can communicate its proximity to asecond attachment 6020 such that, if the first attachment 6020 detectsinterference with one or more of its sensors, the second attachment 6020can understand the source of interference. In at least one suchinstance, the second attachment 6020 can communicate with the firstattachment 6020 and request that the first attachment 6020 depowerand/or otherwise modify its systems to reduce or eliminate the magneticfields being generated by the first attachment 6020. Moreover, thesecond attachment 6020 can communicate with the robotic surgical systemand/or the user to move the first attachment 6020.

In various instances, surgical instrument assemblies are manipulated bya user and/or a surgical robot such that the surgical instrumentassemblies are placed into a variety of orientations that may affect theoperation of the surgical instrument assembly. For example, access tocertain areas of a target site within a patient may be difficult toreach which may result in a surgeon rotating the entire surgicalinstrument assembly into an upside down configuration. In suchinstances, certain operational systems of the surgical instrumentassembly may be affected by such an orientation inversion. With this inmind, various surgical instrument assembles are configured to accountfor such effects. In at least one instance, a surgical instrumentassembly can comprise an orientation-detection system configured todetect the orientation of a surgical instrument assembly and a controlcircuit configured to adjust an operational control program of thesurgical instrument assembly based on the detected orientation of thesurgical instrument assembly.

FIGS. 54 and 55 depict a handheld surgical instrument assembly 5000 anda user 5010 holding the handheld surgical instrument assembly 5000 intwo different orientations. The surgical instrument assembly 5000comprises a handle housing 5020 comprising a grip portion 5030configured to be held by a user 5010 during use and a shaft assembly5040 extending distally from the handle housing 5020. The shaft assembly5040 comprises an end effector configured to treat tissue of a patient.Any suitable end effector can be used such as, for example, a surgicalstapling end effector and/or an energy-based surgical end effector. Thehandle housing 5020 further comprises a trigger 5031 configured toactuate the function of the end effector of the shaft assembly 5040.

The surgical instrument assembly 5000 further comprises anorientation-detection system configured to detect the orientation of thesurgical instrument assembly 5000. Such an orientation-detection systemmay comprise a gyroscopic sensor, for example. In at least one instance,such an orientation-detection system utilizes a camera and/or radartechnology to determine the orientation of the surgical instrumentassembly. FIG. 54 depicts the surgical instrument assembly 5000 in anupright orientation and the user 5010 holding the handle housing 5020 ina standard configuration where the index finger of the user 5010 isconfigured to pull the trigger 5031. The orientation-detection system isconfigured to detect that the surgical instrument assembly 5000 is inthe upright orientation and communicate this information to a controlcircuit. Various embodiments are envisioned which detect the orientationof the handle 5020 relative to gravity. In such instances, the controlsystem can determine that the handle 5020 is in a normal orientationwhen the grip 5030 is extending vertically downwardly or essentiallyvertically downwardly and in an upside-down orientation when the grip5030 is extending vertically upwardly or essentially verticallyupwardly. That said, the shaft of the surgical instrument assembly 5000is rotatable relative to the handle 5020 in various instances and theorientation-detection system can be configured to determine the relativerotation between the shaft and the handle 5020. In such instances, thecontrol system can be configured to alter the control program in someway when the control system determines that the handle 5020 has beenrotated upside-down, or essentially upside-down, relative to the shaft.

The control circuit is configured to adjust an operational controlprogram of the surgical instrument assembly 5000 based on the detectedupright orientation. In at least one instance, the trigger 5031comprises an adjustable component configured to vary the force requiredto squeeze the trigger 5031 to activate a function of the end effector.In at least one instance, a standard force 5050 is required to squeezethe trigger 5031 to activate the function of the end effector when thesurgical instrument assembly 5000 is detected to be in the uprightorientation. Turning now to FIG. 55, the surgical instrument assembly5000 is in an inverted orientation. In the inverted orientation, a user5010 may be holding the grip portion 5030 in an awkward configurationwhich may make it more difficult to apply enough force 5060 to squeezethe trigger 5031 to activate a function of the end effector. In such aninstance, the control circuit is configured to reduce the force requiredto squeeze the trigger 5031 to activate the function of the endeffector. The control circuit is configured to adjust an operationalcontrol program of the surgical instrument assembly 5000 based onergonomics of the surgical instrument assembly 5000 during operationand/or based on varied finger and/or wrist strength during use of thesurgical instrument assembly 5000. In at least one instance, an invertedorientation may reduce operational capabilities of a drive systembecause of the weight of the drive system, for example. In such aninstance, an adjustment can be made to a motor control program torestore the reduced operational capabilities of the drive train to fulloperational capacity based on the inverted orientation. In variousinstances, the control system can reduce the speed of the drive memberbeing actuated, reduce the acceleration, reduce the maximum force,and/or reduce the maximum current that can be drawn by the electricmotor driving the drive member, for example, when the control systemdetermines that the handle is in an inverted orientation. In certaininstances, the control system can modify the time, or pause, betweenoperational steps when a particular orientation is detected. In at leastone instance, the control system can increase the pause between clampingthe end effector and performing a staple firing stroke, for example.

In at least one instance, a control circuit is configured to control aforce threshold required to activate and deactivate a trigger of asurgical instrument assembly. This can allow a user to activate and/ordeactivate the trigger with non-dominate fingers and/or while the handof the user is in a non-dominate configuration, for example.

In various instances, further to the above, the orientation of surgicalstapling end effectors can be detected and a control circuit can adjustan operational control program of the surgical stapling end effectorbased on the detected orientation. FIGS. 56 and 57 depict an endeffector assembly 5100 comprising a shaft 5110 and an end effector 5120extending distally from the shaft 5110. The end effector 5120 comprisesa cartridge jaw 5130 and an anvil jaw 5140 movable relative to thecartridge jaw 5130. While the anvil jaw 5140 is movable in thisembodiment, embodiments are also contemplated where the cartridge jaw5130 is movable in addition to, or in lieu of, the anvil jaw 5140. Theend effector assembly 5100 further comprises an orientation-detectionsystem comprising a gyroscope, for example, configured to detect theorientation of the end effector assembly 5100 relative to gravity.

In at least one instance, the position of the anvil jaw 5140 isdetectable and can be used to determine the orientation of the endeffector assembly 5100. For example, slop can be purposefullyincorporated in the anvil closure drive train to ensure that the anviljaw 5140 falls down into an upright unclamped position (FIG. 57) andfalls down into an inverted unclamped position (FIG. 56) which isdifferent than the upright unclamped position. In such an instance, thedistance between the anvil jaw 5140 and the cartridge jaw 5130 would bedifferent in both orientations; however, the anvil jaw 5140 and thecartridge jaw 5130 would both be in a fully unclamped configuration. Theposition of the anvil jaw 5140 can then be detected to determine theorientation of the end effector assembly 5100.

In at least one instance, a motor is used to rotate the end effectorassembly 5100 about an end effector axis causing the inversion of theend effector assembly 5100. In such an instance, an encoder may beemployed on the motor to determine the orientation of the end effectorassembly 5100.

In at least one instance, the anvil jaw 5140 may require a greater forceto be applied thereto to be opened when the end effector assembly 5100is in the upright orientation (FIG. 57) as compared to the forcerequired to open the anvil jaw 5140 when the end effector assembly 5100is in the inverted orientation (FIG. 56). This may be due to gravitytending to pull the anvil jaw 5140 open relative to the cartridge jaw5130 when the end effector assembly 5100 is in the inverted orientation.When the end effector assembly 5100 is in the upright orientation,gravity will tend to pull the anvil jaw 5140 closed relative to thecartridge jaw 5130. In any event, a control circuit is configured todetect the orientation of the end effector assembly 5100 and makeadjustments to an operational control program based on the force neededto open and/or close the anvil jaw 5140 and/or other parametersdisclosed herein.

In at least one instance, the control circuit is configured toautomatically adjust the position of the anvil jaw 5140 to compensatefor any gravity-based position variance of the anvil jaw 5140 as the endeffector assembly 5100 is moved between various orientations. Forexample, if the anvil jaw 5140 comprises different positions relative tothe cartridge jaw 5130 when the end effector assembly 5100 is indifferent orientations, the control circuit is configured to move theanvil jaw 5140 into a pre-defined unclamped position that matches theunclamped position regardless of the end effector orientation. In suchan instance, the control circuit is configured to eliminate differencesin the unclamped configuration of the anvil jaw 5140 as a result of theorientation of the end effector assembly 5100. In at least one instance,the control circuit is configured to increase force applied to the anviljaw 5140 when the end effector assembly 5100 is in the uprightorientation at least because the anvil jaw 5140 may require more forceto be opened due to gravity working against opening of the anvil jaw5140. In at least one instance, the control circuit is configured todecrease force applied to the anvil jaw 5140 when the end effectorassembly 5100 is in the inverted orientation at least because the anviljaw 5140 may require less force to be opened due to gravity assistingopening of the anvil jaw 5140.

FIGS. 58-61 depict a surgical instrument assembly 5200 comprising anattachment interface 5210, a shaft assembly 5240 attachable to anddetachable from the attachment interface 5210 by way of a shaftattachment adapter 5220, and a sensing system 5230 configured to detectthe orientation of the shaft assembly 5240 relative to the attachmentinterface 5210. The attachment interface 5210 may comprise any suitableattachment interface such as, for example, a surgical robot and/or ahandheld surgical housing. The attachment interface 5210 compriseselectrical contacts 5211 configured to electrically couple contacts 5221of the shaft attachment adapter 5220 with the attachment interface 5210.

The shaft assembly 5240 comprises a shaft 5250 and an electricalattachment mechanism 5260 positioned on a proximal end of the shaftassembly 5240. The electrical attachment mechanism 5260 compriseselectrical contacts 5261 and electrical leads 5263 extending distallyfrom the electrical contacts 5261. The shaft assembly 5240 comprises atleast one electrical system downstream of the electrical attachmentmechanism 5260 with which the electrical contacts 5261 are coupled. Theshaft assembly 5240 is configured to be physically and electricallycoupled with the shaft attachment adapter 5220 by the electricalattachment mechanism 5260 and the sensing system 5230 comprises a slipring assembly which places the shaft assembly 5240 in communication withthe attachment adapter 5220.

The sensing system 5230 is configured to determine the orientation ofthe shaft assembly 5240 relative to the attachment interface 5210. Thesensing system 5230 comprises an outer slip ring 5231, an intermediateslip ring 5233, and an inner slip ring 5235. The contacts 5261 areconfigured to be electrically coupled with the attachment interface 5210through the slip rings 5231, 5233, 5235. The slip rings 5231, 5233, 5235each comprise a discontinuity therein. The outer slip ring 5231comprises an outer discontinuity 5232, the intermediate ring 5233comprises an intermediate discontinuity 5234, and the inner slip ring5235 comprises an inner discontinuity 5236. The discontinuities 5232,5234, 5236 are used to determine the orientation of the end shaftassembly 5240 as the shaft assembly 5240 is rotated relative to theshaft attachment adapter 5220. When the shaft assembly 5240 is rotated,the contacts 5261 pass over the discontinuities 5232, 5234, 5236.

In at least one instance, the discontinuities 5232, 5234, 5236 comprisehigh resistance regions that are detectable within the electricalcircuit. As the contacts 5261 pass over the discontinuities 5232, 5234,5236, high resistance can be detected. A control circuit is configuredto keep track of how many times and in what order the contacts 5261 passover the high resistance regions as the shaft assembly 5240 is rotatedrelative to the shaft attachment adapter 5230. The control circuit isconfigured to determine what orientation the shaft assembly 5140 is inrelative to the shaft attachment adapter 5220 based on the number oftimes the contacts 5261 pass over the discontinuities 5232, 5234, 5236.

FIG. 59 depicts the shaft assembly 5240 in an upright orientation. Asthe shaft assembly 5240 is rotated counterclockwise into the orientationillustrated in FIG. 60, a control circuit can determine that thecontacts 5261 passed over the outer discontinuity 5232 based on a highresistance detection, for example, within a circuit including the outerslip ring 5231. Because the outer discontinuity 5232 was passed overfirst, as opposed to the other discontinuities 5234 and 5236, thecontrol circuit can determine which direction the shaft assembly 5240was rotated. As can be seen in FIG. 60, the shaft assembly 5240 has beenrotated counterclockwise into an inverted orientation from theorientation illustrated in FIG. 59. Rotating into this position willcause the intermediate discontinuity 5234 to be passed over. As aresult, the control circuit can determine that the shaft assembly 5240is inverted based on the fact that the outer discontinuity 5232 wasfirst detected and then the intermediate discontinuity 5234 wasdetected.

In at least one instance, slip rings of surgical instrument assembliescomprise high conductivity regions as well as low conductivity regions.In such an instance, the control circuit is configured to determine whenthe shaft assembly has rotated to and settled on a low conductivityregion. This may be disadvantageous when trying to preserve theelectrical communication between the attachment interface and anyelectric system within the shaft assembly. In such an instance, thecontrol circuit is configured to adjust an operational control programwhich controls the rotation of the shaft assembly relative to theattachment interface to which the shaft assembly is attached. In atleast one instance, the operational control program is adjusted so thatthe shaft assembly is rotated out of the low conductive regions andimmediately into the nearest high conductivity region. In at least oneinstance, a user is alerted of the low conductivity relationship betweenthe shaft assembly and the attachment interface. In such an instance,the user can adjust the shaft assembly manually and/or ignore the alertregarding the detected low conductivity relationship.

In at least one instance, a control circuit is configured to logconductivity issues of different components and the areas in which thereare conductivity problems. In at least one instance, a component can belocked out after a certain threshold of low conductivity regions hasbeen detected. In such an instance, if the component is ever re-attachedwithin a surgical instrument system, the control circuit can alert auser of the situation and/or lock out the component from being used.

In at least one instance, such an orientation-detection system can beused with an energy-based surgical device. In such an instance, acontrol circuit is configured to limit generator power delivered throughthe components when a low conductivity relationship is present. In atleast one instance, the electrical circuits are used for sensingsystems. In such instances, the control circuit is configured to ignoresignals transmitted when a low conductivity relationship is present.

In various instances, a control circuit is provided to adjust anoperational control program of a surgical instrument assembly and/orrobot, for example, based on a detected orientation of a patient. FIGS.62-64 depict a surgical instrument system 5300 comprising a patient 5310and an operating table 5320 on which the patient 5310 is positioned forsurgery. The surgical instrument system 5300 further comprises anorientation-detection system such as a gyroscopic sensor, for example,configured to detect the orientation of the patient. A control circuitis provided to adjust operational control parameters of surgicalinstrument assemblies and systems used during surgery based on thedetected orientation of the patient. In at least one instance,adjustments are made such that positional limits are placed on whererobotic arms can move relative to the patient based on the patient'sdetected orientation. For example, if the patient is in the orientationdepicted in FIG. 62, the control circuit may limit movement of roboticarms such that the robotic arms do not move below the patient where therobotic arms may not be useful and/or harm the patient.

In various instances, a surgical hub is used within a surgicalenvironment. The surgical hub is configured to communicate with one ormore modules within the surgical environment. The modules may compriseshaft assemblies, end effectors, surgical instrument handles, surgicalrobots, operating tables, and/or robotic control interfaces, forexample. The surgical hub may be connected to a cloud-based system. Thesurgical hub is configured to communicate with the modules to determinevarious characteristics of the modules. The surgical hub is alsoconfigured to control operational capabilities of each module.

FIG. 65 is a flow chart 7000 depicting a surgical instrument controlcircuit for use in an environment with modular surgical instrumentcomponents and/or a surgical hub. The control circuit is configured toreceive a plurality of hardware inputs 7010 comprising information aboutmodular surgical instrument components and/or the surgical hub. Theinputs may comprise capability information of each module, for example.The control circuit is also configured to identify various parameters7020 of the surgical environment. The various parameters 7020 compriseidentification of possible component assembly combinations,identification of patient data corresponding to the intended surgery,for example, identification of procedural parameters, and identificationof business parameters. In at least one instance, the control circuit isfurther configured to consider what surgeon is executing the surgery,what operating room the surgery is taking place, and/or what hospitalthe surgery is taking. All such inputs and parameters can affect how themodules and the surgical hub operate.

The control circuit is further configured to determine recommendedsolutions 7030 based on all of the inputs received by the controlcircuit. The recommended solutions 7030 may comprise optimal operationalcontrol programs for motors within various modules and/or sensingcontrol programs configured optimize sensing capabilities of sensingsystems within the modules. In at least one instance, the controlcircuit is configured to provide optional solutions 7040 to a user. Theoptional solutions 7040 comprise a first solution that comprises acontrol program that utilizes a multi-axis articulation system of amodule. The optional solutions 7040 also comprises a second solutionthat comprises a control program that limits the multi-axis articulationsystem of the module to single-axis. In at least one instance, a user isconfigured to choose 7050 the desired solution. In at least oneinstance, a manual lockout 7060 is provided. In at least one instance,if the user chooses the optional solution 7040 utilizing single-axisarticulation, then the control circuit is configured to lockoutmulti-axis articulation of the module.

In various instances, a control circuit is configured to identify allsub systems and/or components within a surgical hub environment. In atleast one instance, modules configured to be used in the surgical hubenvironment each comprise means or wireless communicating with thesurgical hub. In at least one instance, the control circuit isconfigured to identify each module within the surgical hub environment.In at least one instance, the control circuit is configured to define anoperational control program for each module identified within thesurgical hub environment.

In various instances, a control circuit is configured to identify allsub-systems within a surgical hub environment and automatically evaluateeach identified sub-system. The evaluation may include runninginitialization programs to operate through all drive systems and/orsensing systems onboard each sub-system. In at least one instance, thecontrol circuit is configured to connect each sub-system wirelessly toevery other sub-system such that the sub-systems are able to communicatewith each other. In at least one instance, the control circuit isconfigured to connect each sub-system to a surgical hub.

In at least one instance, a control circuit is configured actuatethrough each drive system of a combination of connected sub-systems.This actuation can be used to determine the capabilities of thecombination of the connected sub-systems. In at least one instance, thecontrol circuit is configured to adjust an operational control programbased on feedback received during the initial actuation of thecombination of connected sub-systems. In at least one instance, thecontrol circuit is configured to compare the received feedback withinformation collected during previous uses of each sub-system. In suchan instance, the control circuit can determine what portion of anyoperational variance is due to the combination of the connectedsub-systems or is due to each sub-system itself. For example, a shaftassembly and an end effector assembly may be attached to each otherforming a modular instrument assembly. The modular instrument assemblymay then be attached to a handheld motorized attachment interface. Thehandheld motorized attachment interface may then automatically runthrough an initialization actuation phase to determine the availablefunctions of the modular instrument assembly.

In various instances, a control circuit is configured to identify eachmodule within a surgical hub environment and, based on the one or moreidentified modules, determine all possible combinations and/orsub-combinations of the identified modules. This may be determined bypermissible pre-determined combinations. In at least one instance, auser can be displayed the various options of combinations availablebetween all of the identified modules. In at least one instance, thecontrol circuit is configured to recommend one or more modulecombinations based on the permissible pre-determined combinations and/orbased on other inputs such as, for example, patient data and/or surgeonexpertise level.

In various instances, a surgical instrument system comprises a remoteserver configured to aggregate different combinations of parts,tolerances, assembly modifications, and/or performance statistics frommodules in the field. In at least one instance, a control circuit isconfigured to determine operational control parameters for any specificcombination of modules. In at least one instance, the control circuit isconfigured to communicate the determined operational control parametersto all other modules. In at least one instance, the control circuit isconfigured to communicate the determined operational control parametersto other similar combinations of modules in the field. In at least oneinstance, the aggregation comprises a constantly evolving algorithm and,as more data and/or information is collected further defining thepossible combinations, the control circuit can continuously iterate thepossible combinations.

In at least one instance, the iteration process may comprise providingone possible solution to a first module system and a second possiblesolution to a second module system with similar variances and then usethe outcomes of the first module system and the second module system tofurther refine the control parameters for the general population ofmodules. If an issue is identified with a specific combination isidentified, the control circuit may notify a user of the issue. In atleast one instance, the control circuit is configured to lockout thespecific combination of modules when an issue with a specificcombination of modules is detected. In at least one instance, a user mayoverride the locked out combination and, with the understanding of whatthe identified issue is, the control circuit can unlock the modulecombination device. In such an instance, the control circuit isconfigured to more closely monitor usage data than would be monitoredduring normal use to allow for post-use diagnostics.

In at least one instance, calibration parameters are stored within eachmodule onboard a local memory, for example. In at least one instance,other adjustment factors may be uploaded to the module itself such thatthe next time the module is connected to another module and/or thesurgical hub, the other modules and/or the surgical hub can recognizethe change in calibration parameters of the module. In variousinstances, the surgical hub is configured to utilize identification datareceived from each module such as, for example, serial numbers to lookup viable control algorithms and/or operational parameters, for examplefor the specific module. In at least one embodiment, adjustment factorsfrom two or more attached components are uploaded to the module and/orsurgical hub. In such embodiments, the performance of the system can beco-operatively altered by two or more sets of adjustment parameter sets.

In at least one instance, a control circuit is configured to adjust avariety of control parameters such as, for example, a pause time betweenactuating various systems of a module, how long to wait before taking ameasurement with an onboard sensing system of the module, minimum andmaximum threshold limits related to motor speed and/or energy delivery,for example, stroke length of an actuation system of the module,actuation speeds of actuation systems of the module, initial actuationforce of the module, rate of change trigger thresholds, and/or magnitudeof rate of change adjustments. In at least one instance, controlparameters are adjusted based on whether a cartridge with an adjunctpre-installed on the cartridge is present or a cartridge without anadjunct is present. In at least one instance, control parameters areadjusted based on the size of staples stored within the cartridge modulethat is installed.

FIG. 66 is a schematic of a surgical instrument system 8000 comprising asurgical hub 8010, a data cloud 8020, a handheld actuation module 8030,and a shaft assembly module 8040. Each module 8030, 8040 comprises anRFID communication device configured to allow intercommunication betweenthe modules 8030, 8040 and the surgical hub 8010. The data cloud 8020 isconfigured to store software program data, situational awareness data,and/or any suitable hub data therein. The surgical hub 8010 isconfigured to access the data cloud 8020 to determine if various modulesbeing used require a reduced functionality for any given set of data inthe data cloud 8020. In at least one instance, the shaft assembly module8040 comprises a smart battery and/or a smart display.

In at least one instance, the operational capabilities of a moduleinclude a degree of end effector articulation of an end effectorassembly, energy output levels of an energy-based surgical device,and/or speed of staple firing of a surgical stapling shaft assembly, forexample. End effector articulation, for example, may be reduced to arange of 45 degrees left and 45 degrees right from a full articulationrange of an end effector assembly which may be 90 degrees left and 90degrees right, for example. Energy output levels, for example, may bereduced to lower power levels than what an energy-based surgical deviceis capable of delivering to a patient, for example. Speed of staplefiring of a surgical stapling shaft assembly may be reduced to halfspeed, for example.

In various instances, a surgical hub is configured to identify a modulewithin the surgical environment. In at least one instance, the surgicalhub is configured to determine the capabilities of the module byinterpreting a signal received from the module which may include datacorresponding to the capabilities of the module. The surgical hub isconfigured to limit the capabilities of the module based on apre-defined control program. The pre-defined control program may bedefined by a level of software package purchased for the module. Forexample, there may exist three different levels of software. The levelsmay comprise, for example, beginner, intermediate, and/or advanced. Ifthe beginner level of software is purchased, the capabilities of themodule may be reduced to a beginner configuration. Such a configurationmay include slowing the firing speed and/or reducing range ofarticulation, for example. If the intermediate level of software ispurchased, the capabilities of the module may be increased from thebeginner configuration to an intermediate configuration where the moduleis not able to run in at a full capabilities configuration but, rather,the intermediate configuration. Such a configuration may includeproviding the full range of articulation but maintaining the reducedfiring speed. If the advanced level of software is purchased, thecapabilities of the module may be at a maximum capability configurationwhere every feature is unlocked and able to be used and/or the module isable to run at the full capabilities configuration.

Such software level upgrades may be employed in a training environmentwhere it may be safer to limit certain surgeons to a more beginner levelof software. The surgical hub may track the surgeons while using thebeginner level of software and determine when the surgeons are ready toadvance to the next level. The surgical hub may alert a surgeon of anavailable upgrade in software level and/or automatically upgrade themodule for that particular surgeon. Different surgeons may bedifferentiated by using login information within the surgical hub suchthat one more advanced surgeon may be able to use a module at a moreadvanced software level while the more advanced surgeon is logged in tothe surgical hub and another more beginner surgeon may be limited tousing that same module at a more beginner software level while thebeginner surgeon is logged in to the surgical hub.

In at least one instance, the surgical hub is configured to enablefeatures and/or full capabilities of a module on-the-fly. For example,an override feature may be provided such that a surgeon is able tooverride a system restricting the surgeon to certain capabilities.

In at least one instance, the surgical hub is configured to determinethe appropriate level of shaft capabilities based on patient dataaccessible by the surgical hub from the cloud-based system. For example,a certain patient may not need high energy levels based on the type oftissue expected to be operated on. In such an instance, the surgical hubis configured to limit the energy delivery levels of an energy-basedsurgical instrument module for that patient's surgery. In at least oneinstance, available functionality of an energy-based surgical instrumentmodule is defined and/or limited based on available power within asurgical suite. For example, a previous generation generator may be theonly source of power for the energy-based surgical instrument modulethat may not be able to deliver enough power to maximize the potentialof the energy-based surgical instrument module. In such an instance, theenergy-based surgical instrument module is limited to a low-powerconfiguration. In at least one instance, available power within thesurgical suite may be limited and a surgical instrument generator,itself, may be placed into a low-power operational mode based on theavailability of power within the surgical suite.

In at least one instance, capabilities of module configured to beenabled and/or limited may include sensing systems. If a surgeon isunfamiliar with how a more advanced and/or precise sensing system workswithin a particular module, for example, that sensing system may beentirely disabled for that surgeon. In at least one instance, thesensing system is placed into a training mode that allows a surgeon tolearn how the sensing system works before the sensing system operates ata full capabilities level. In at least one instance, the sensing systemis operated at a reduced state to simply the module for the surgeon.

In at least one instance, the surgical hub is configured to send a test,or initialization, signal to each module to determine each module'srange of capabilities and limits. This may also be referred to as amodule-interrogation stage, for example. In at least one instance, thesurgical hub is also configured to determine any irregularities and/orworn systems, for example, within each module during the test program.In at least one instance, an initialization signal is sent to eachmodule to be used during a surgery prior to the surgery commencing. Inat least one instance, the initialization signal is sent to each modulejust before the module is used during the surgery. In at least oneinstance, the surgical hub is configured to alert a user if any of themodules need replaced based on detected irregularities, for example.Irregularities may be detected by onboard sensing systems of eachmodule. During an initialization stage, an onboard motor, for example,is configured to actuate through all systems and test all actuationsystems and/or sensing systems onboard a module. In modules without amotor, such initialization may occur once the module is attached to amotorized actuation system. In such an instance, the module may belocked out from regular use during the initialization stage.

In at least one instance, a motorized actuation module, such as ahandheld attachment interface to which various shaft assemblies and/orend effectors may be attached, is used to limit capabilities of thevarious shaft assemblies and/or end effectors attached to the motorizedactuation module. For example, a shaft assembly to be attached to themotorized actuation module may not comprise a communication means tocommunicate with the hub. In such an instance, a control program of themotorized actuation module is defined to limit and/or define theavailable functionality of the shaft assembly.

In at least one instance, module functionality may be defined based onhow many times the module has been used. Such data can be kept withinthe module itself locally. In at least one instance, the surgical hub isconfigured to track how many times a particular module has been used. Inat least one instance, module functionality may be defined by the age ofthe module. In at least one instance, module functionality may bedefined by the age of a power source. In at least one instance, modulefunctionality may be defined by events logged during previous uses ofthe module. In at least one instance, the events logged may includeproblematic uses where one or more systems within the module failedduring use, for example. For example, during a first use, anarticulation drive system of a surgical stapling end effector module maybreak. The surgical hub is configured to log this event. A surgeon mayreattach the surgical stapling end effector module knowing that thearticulation system is broken. The surgical hub may limit and/or lockoutthe use of the articulation drive system and permit the surgeon to usethe clamping, stapling, and/or cutting functions only.

In various instances, modules and a surgical hub may comprise a level ofintercommunication that is controllable based on cost and/or needs, forexample. In at least one instance, various modules comprise capablecommunication array systems configured to communicate with the surgicalhub and/or other modules with capable communication array systems. In atleast one instance, the level of intercommunication between modulesand/or the surgical hub may be reduced based on the purchased software.To unlock full intercommunication, an advanced communication softwaremay have to be purchased.

A first tier intercommunication level could provide basic communicationbetween each module and the hub. For example, with the first tierintercommunication level, each module may be able to transmitinformation to the surgical hub; however, with the first tierintercommunication level, the modules may not be able to communicatewith each other nor would the surgical hub be able to send upgradesignals, for example, to the modules. A second tier intercommunicationlevel could, in addition to the capabilities of the first tierintercommunication level, provide the surgical hub with the ability tosend update signals to updateable modules. A third tierintercommunication level could provide full intercommunication betweenall capable modules and the surgical hub unlocking full access tosoftware updates, module intercommunication, and/or logging device usagestatistics, for example.

In at least one instance, upgrading system software of various modulescan be advantageous as control programs are used multiple times after aninitial roll out of a local module. The surgical hub can be configuredto update operational algorithms of a local module based on usage of themodule in multiple different hospitals, for example. All of the usagestatistics of the uses of the module in the multiple different hospitalscan be logged and used to update the operational algorithms of themodule. Updating the software of the local module regularly can updatethe operational algorithm of the local module providing a safer and/ormore effective operational algorithm for the local module.

In at least one instance, multiple different software programs existwithin the surgical hub. A first software program is configured tocontain all of the information corresponding to full functionality of amodule such as a shaft assembly, for example. A second software programsuch as, an add on, for example, may be available which containsadvanced modes such as, for example, a power limiting mode, a sleepmode, an increased core kernel processing mode which may allow a moduleto take more precise measurements, take more measurements, react faster,and/or operate faster and/or more efficiently, for example. In at leastone instance, the different software programs are selectable by a user.In at least one instance, the cost paid for a module corresponds towhich software program is available for that module. In at least oneinstance, software programs are readily updateable for a module. In atleast one instance, the surgical hub is configured to recommend asoftware program based on situational awareness data within the hub.

Many of the surgical instrument systems described herein are motivatedby an electric motor; however, the surgical instrument systems describedherein can be motivated in any suitable manner. In various instances,the surgical instrument systems described herein can be motivated by amanually-operated trigger, for example. In certain instances, the motorsdisclosed herein may comprise a portion or portions of a roboticallycontrolled system. Any of the systems disclosed herein can be used witha handled surgical instrument. Moreover, any of the systems disclosedherein can be utilized with a robotic surgical instrument system. U.S.patent application Ser. No. 13/118,241, entitled SURGICAL STAPLINGINSTRUMENTS WITH ROTATABLE STAPLE DEPLOYMENT ARRANGEMENTS, now U.S. Pat.No. 9,072,535, for example, discloses several examples of a roboticsurgical instrument system in greater detail and is incorporated byreference herein in its entirety.

The surgical instrument systems described herein have been described inconnection with the deployment and deformation of staples; however, theembodiments described herein are not so limited. Various embodiments areenvisioned which deploy fasteners other than staples, such as clamps ortacks, for example. Moreover, various embodiments are envisioned whichutilize any suitable means for sealing tissue. For instance, an endeffector in accordance with various embodiments can comprise electrodesconfigured to heat and seal the tissue. Also, for instance, an endeffector in accordance with certain embodiments can apply vibrationalenergy to seal the tissue.

Various embodiments described herein are described in the context oflinear end effectors and/or linear fastener cartridges. Suchembodiments, and the teachings thereof, can be applied to non-linear endeffectors and/or non-linear fastener cartridges, such as, for example,circular and/or contoured end effectors. For example, various endeffectors, including non-linear end effectors, are disclosed in U.S.patent application Ser. No. 13/036,647, filed Feb. 28, 2011, entitledSURGICAL STAPLING INSTRUMENT, now U.S. Patent Application PublicationNo. 2011/0226837, now U.S. Pat. No. 8,561,870, which is herebyincorporated by reference in its entirety. Additionally, U.S. patentapplication Ser. No. 12/893,461, filed Sep. 29, 2012, entitled STAPLECARTRIDGE, now U.S. Patent Application Publication No. 2012/0074198, ishereby incorporated by reference in its entirety. U.S. patentapplication Ser. No. 12/031,873, filed Feb. 15, 2008, entitled ENDEFFECTORS FOR A SURGICAL CUTTING AND STAPLING INSTRUMENT, now U.S. Pat.No. 7,980,443, is also hereby incorporated by reference in its entirety.U.S. Pat. No. 8,393,514, entitled SELECTIVELY ORIENTABLE IMPLANTABLEFASTENER CARTRIDGE, which issued on Mar. 12, 2013, is also herebyincorporated by reference in its entirety.

The entire disclosures of:

-   -   U.S. Pat. No. 5,403,312, entitled ELECTROSURGICAL HEMOSTATIC        DEVICE, which issued on Apr. 4, 1995;    -   U.S. Pat. No. 7,000,818, entitled SURGICAL STAPLING INSTRUMENT        HAVING SEPARATE DISTINCT CLOSING AND FIRING SYSTEMS, which        issued on Feb. 21, 2006;    -   U.S. Pat. No. 7,422,139, entitled MOTOR-DRIVEN SURGICAL CUTTING        AND FASTENING INSTRUMENT WITH TACTILE POSITION FEEDBACK, which        issued on Sep. 9, 2008;    -   U.S. Pat. No. 7,464,849, entitled ELECTRO-MECHANICAL SURGICAL        INSTRUMENT WITH CLOSURE SYSTEM AND ANVIL ALIGNMENT COMPONENTS,        which issued on Dec. 16, 2008;    -   U.S. Pat. No. 7,670,334, entitled SURGICAL INSTRUMENT HAVING AN        ARTICULATING END EFFECTOR, which issued on Mar. 2, 2010;    -   U.S. Pat. No. 7,753,245, entitled SURGICAL STAPLING INSTRUMENTS,        which issued on Jul. 13, 2010;    -   U.S. Pat. No. 8,393,514, entitled SELECTIVELY ORIENTABLE        IMPLANTABLE FASTENER CARTRIDGE, which issued on Mar. 12, 2013;    -   U.S. patent application Ser. No. 11/343,803, entitled SURGICAL        INSTRUMENT HAVING RECORDING CAPABILITIES, now U.S. Pat. No.        7,845,537;    -   U.S. patent application Ser. No. 12/031,573, entitled SURGICAL        CUTTING AND FASTENING INSTRUMENT HAVING RF ELECTRODES, filed        Feb. 14, 2008;    -   U.S. patent application Ser. No. 12/031,873, entitled END        EFFECTORS FOR A SURGICAL CUTTING AND STAPLING INSTRUMENT, filed        Feb. 15, 2008, now U.S. Pat. No. 7,980,443;    -   U.S. patent application Ser. No. 12/235,782, entitled        MOTOR-DRIVEN SURGICAL CUTTING INSTRUMENT, now U.S. Pat. No.        8,210,411;    -   U.S. patent application Ser. No. 12/235,972, entitled MOTORIZED        SURGICAL INSTRUMENT, now U.S. Pat. No. 9,050,083.    -   U.S. patent application Ser. No. 12/249,117, entitled POWERED        SURGICAL CUTTING AND STAPLING APPARATUS WITH MANUALLY        RETRACTABLE FIRING SYSTEM, now U.S. Pat. No. 8,608,045;    -   U.S. patent application Ser. No. 12/647,100, entitled        MOTOR-DRIVEN SURGICAL CUTTING INSTRUMENT WITH ELECTRIC ACTUATOR        DIRECTIONAL CONTROL ASSEMBLY, filed Dec. 24, 2009, now U.S. Pat.        No. 8,220,688;    -   U.S. patent application Ser. No. 12/893,461, entitled STAPLE        CARTRIDGE, filed Sep. 29, 2012, now U.S. Pat. No. 8,733,613;    -   U.S. patent application Ser. No. 13/036,647, entitled SURGICAL        STAPLING INSTRUMENT, filed Feb. 28, 2011, now U.S. Pat. No.        8,561,870;    -   U.S. patent application Ser. No. 13/118,241, entitled SURGICAL        STAPLING INSTRUMENTS WITH ROTATABLE STAPLE DEPLOYMENT        ARRANGEMENTS, now U.S. Pat. No. 9,072,535;    -   U.S. patent application Ser. No. 13/524,049, entitled        ARTICULATABLE SURGICAL INSTRUMENT COMPRISING A FIRING DRIVE,        filed on Jun. 15, 2012, now U.S. Pat. No. 9,101,358;    -   U.S. patent application Ser. No. 13/800,025, entitled STAPLE        CARTRIDGE TISSUE THICKNESS SENSOR SYSTEM, filed on Mar. 13,        2013, now U.S. Pat. No. 9,345,481;

U.S. patent application Ser. No. 13/800,067, entitled STAPLE CARTRIDGETISSUE THICKNESS SENSOR SYSTEM, filed on Mar. 13, 2013, now U.S. PatentApplication Publication No. 2014/0263552;

-   -   U.S. Patent Application Publication No. 2007/0175955, entitled        SURGICAL CUTTING AND FASTENING INSTRUMENT WITH CLOSURE TRIGGER        LOCKING MECHANISM, filed Jan. 31, 2006; and    -   U.S. Patent Application Publication No. 2010/0264194, entitled        SURGICAL STAPLING INSTRUMENT WITH AN ARTICULATABLE END EFFECTOR,        filed Apr. 22, 2010, now U.S. Pat. No. 8,308,040, are hereby        incorporated by reference herein.

Although various devices have been described herein in connection withcertain embodiments, modifications and variations to those embodimentsmay be implemented. Particular features, structures, or characteristicsmay be combined in any suitable manner in one or more embodiments. Thus,the particular features, structures, or characteristics illustrated ordescribed in connection with one embodiment may be combined in whole orin part, with the features, structures or characteristics of one or moreother embodiments without limitation. Also, where materials aredisclosed for certain components, other materials may be used.Furthermore, according to various embodiments, a single component may bereplaced by multiple components, and multiple components may be replacedby a single component, to perform a given function or functions. Theforegoing description and following claims are intended to cover allsuch modification and variations.

The devices disclosed herein can be designed to be disposed of after asingle use, or they can be designed to be used multiple times. In eithercase, however, a device can be reconditioned for reuse after at leastone use. Reconditioning can include any combination of the stepsincluding, but not limited to, the disassembly of the device, followedby cleaning or replacement of particular pieces of the device, andsubsequent reassembly of the device. In particular, a reconditioningfacility and/or surgical team can disassemble a device and, aftercleaning and/or replacing particular parts of the device, the device canbe reassembled for subsequent use. Those skilled in the art willappreciate that reconditioning of a device can utilize a variety oftechniques for disassembly, cleaning/replacement, and reassembly. Use ofsuch techniques, and the resulting reconditioned device, are all withinthe scope of the present application.

The devices disclosed herein may be processed before surgery. First, anew or used instrument may be obtained and, when necessary, cleaned. Theinstrument may then be sterilized. In one sterilization technique, theinstrument is placed in a closed and sealed container, such as a plasticor TYVEK bag. The container and instrument may then be placed in a fieldof radiation that can penetrate the container, such as gamma radiation,x-rays, and/or high-energy electrons. The radiation may kill bacteria onthe instrument and in the container. The sterilized instrument may thenbe stored in the sterile container. The sealed container may keep theinstrument sterile until it is opened in a medical facility. A devicemay also be sterilized using any other technique known in the art,including but not limited to beta radiation, gamma radiation, ethyleneoxide, plasma peroxide, and/or steam.

While several forms have been illustrated and described, it is not theintention of Applicant to restrict or limit the scope of the appendedclaims to such detail. Numerous modifications, variations, changes,substitutions, combinations, and equivalents to those forms may beimplemented and will occur to those skilled in the art without departingfrom the scope of the present disclosure. Moreover, the structure ofeach element associated with the described forms can be alternativelydescribed as a means for providing the function performed by theelement. Also, where materials are disclosed for certain components,other materials may be used. It is therefore to be understood that theforegoing description and the appended claims are intended to cover allsuch modifications, combinations, and variations as falling within thescope of the disclosed forms. The appended claims are intended to coverall such modifications, variations, changes, substitutions,modifications, and equivalents.

The foregoing detailed description has set forth various forms of thedevices and/or processes via the use of block diagrams, flowcharts,and/or examples. Insofar as such block diagrams, flowcharts, and/orexamples contain one or more functions and/or operations, it will beunderstood by those within the art that each function and/or operationwithin such block diagrams, flowcharts, and/or examples can beimplemented, individually and/or collectively, by a wide range ofhardware, software, firmware, or virtually any combination thereof.Those skilled in the art will recognize that some aspects of the formsdisclosed herein, in whole or in part, can be equivalently implementedin integrated circuits, as one or more computer programs running on oneor more computers (e.g., as one or more programs running on one or morecomputer systems), as one or more programs running on one or moreprocessors (e.g., as one or more programs running on one or moremicroprocessors), as firmware, or as virtually any combination thereof,and that designing the circuitry and/or writing the code for thesoftware and or firmware would be well within the skill of one of skillin the art in light of this disclosure. In addition, those skilled inthe art will appreciate that the mechanisms of the subject matterdescribed herein are capable of being distributed as one or more programproducts in a variety of forms, and that an illustrative form of thesubject matter described herein applies regardless of the particulartype of signal bearing medium used to actually carry out thedistribution.

Instructions used to program logic to perform various disclosed aspectscan be stored within a memory in the system, such as dynamic randomaccess memory (DRAM), cache, flash memory, or other storage.Furthermore, the instructions can be distributed via a network or by wayof other computer readable media. Thus a machine-readable medium mayinclude any mechanism for storing or transmitting information in a formreadable by a machine (e.g., a computer), but is not limited to, floppydiskettes, optical disks, compact disc, read-only memory (CD-ROMs), andmagneto-optical disks, read-only memory (ROMs), random access memory(RAM), erasable programmable read-only memory (EPROM), electricallyerasable programmable read-only memory (EEPROM), magnetic or opticalcards, flash memory, or a tangible, machine-readable storage used in thetransmission of information over the Internet via electrical, optical,acoustical or other forms of propagated signals (e.g., carrier waves,infrared signals, digital signals, etc.). Accordingly, thenon-transitory computer-readable medium includes any type of tangiblemachine-readable medium suitable for storing or transmitting electronicinstructions or information in a form readable by a machine (e.g., acomputer).

As used in any aspect herein, the term “control circuit” may refer to,for example, hardwired circuitry, programmable circuitry (e.g., acomputer processor including one or more individual instructionprocessing cores, processing unit, processor, microcontroller,microcontroller unit, controller, digital signal processor (DSP),programmable logic device (PLD), programmable logic array (PLA), orfield programmable gate array (FPGA)), state machine circuitry, firmwarethat stores instructions executed by programmable circuitry, and anycombination thereof. The control circuit may, collectively orindividually, be embodied as circuitry that forms part of a largersystem, for example, an integrated circuit (IC), an application-specificintegrated circuit (ASIC), a system on-chip (SoC), desktop computers,laptop computers, tablet computers, servers, smart phones, etc.Accordingly, as used herein “control circuit” includes, but is notlimited to, electrical circuitry having at least one discrete electricalcircuit, electrical circuitry having at least one integrated circuit,electrical circuitry having at least one application specific integratedcircuit, electrical circuitry forming a general purpose computing deviceconfigured by a computer program (e.g., a general purpose computerconfigured by a computer program which at least partially carries outprocesses and/or devices described herein, or a microprocessorconfigured by a computer program which at least partially carries outprocesses and/or devices described herein), electrical circuitry forminga memory device (e.g., forms of random access memory), and/or electricalcircuitry forming a communications device (e.g., a modem, communicationsswitch, or optical-electrical equipment). Those having skill in the artwill recognize that the subject matter described herein may beimplemented in an analog or digital fashion or some combination thereof.

As used in any aspect herein, the term “logic” may refer to an app,software, firmware and/or circuitry configured to perform any of theaforementioned operations. Software may be embodied as a softwarepackage, code, instructions, instruction sets and/or data recorded onnon-transitory computer readable storage medium. Firmware may beembodied as code, instructions or instruction sets and/or data that arehard-coded (e.g., nonvolatile) in memory devices.

As used in any aspect herein, the terms “component,” “system,” “module”and the like can refer to a computer-related entity, either hardware, acombination of hardware and software, software, or software inexecution.

As used in any aspect herein, an “algorithm” refers to a self-consistentsequence of steps leading to a desired result, where a “step” refers toa manipulation of physical quantities and/or logic states which may,though need not necessarily, take the form of electrical or magneticsignals capable of being stored, transferred, combined, compared, andotherwise manipulated. It is common usage to refer to these signals asbits, values, elements, symbols, characters, terms, numbers, or thelike. These and similar terms may be associated with the appropriatephysical quantities and are merely convenient labels applied to thesequantities and/or states.

A network may include a packet switched network. The communicationdevices may be capable of communicating with each other using a selectedpacket switched network communications protocol. One examplecommunications protocol may include an Ethernet communications protocolwhich may be capable permitting communication using a TransmissionControl Protocol/Internet Protocol (TCP/IP). The Ethernet protocol maycomply or be compatible with the Ethernet standard published by theInstitute of Electrical and Electronics Engineers (IEEE) titled “IEEE802.3 Standard”, published in December, 2008 and/or later versions ofthis standard. Alternatively or additionally, the communication devicesmay be capable of communicating with each other using an X.25communications protocol. The X.25 communications protocol may comply orbe compatible with a standard promulgated by the InternationalTelecommunication Union-Telecommunication Standardization Sector(ITU-T). Alternatively or additionally, the communication devices may becapable of communicating with each other using a frame relaycommunications protocol. The frame relay communications protocol maycomply or be compatible with a standard promulgated by ConsultativeCommittee for International Telegraph and Telephone (CCITT) and/or theAmerican National Standards Institute (ANSI). Alternatively oradditionally, the transceivers may be capable of communicating with eachother using an Asynchronous Transfer Mode (ATM) communications protocol.The ATM communications protocol may comply or be compatible with an ATMstandard published by the ATM Forum titled “ATM-MPLS NetworkInterworking 2.0” published August 2001, and/or later versions of thisstandard. Of course, different and/or after-developedconnection-oriented network communication protocols are equallycontemplated herein.

Unless specifically stated otherwise as apparent from the foregoingdisclosure, it is appreciated that, throughout the foregoing disclosure,discussions using terms such as “processing,” “computing,”“calculating,” “determining,” “displaying,” or the like, refer to theaction and processes of a computer system, or similar electroniccomputing device, that manipulates and transforms data represented asphysical (electronic) quantities within the computer system's registersand memories into other data similarly represented as physicalquantities within the computer system memories or registers or othersuch information storage, transmission or display devices.

One or more components may be referred to herein as “configured to,”“configurable to,” “operable/operative to,” “adapted/adaptable,” “ableto,” “conformable/conformed to,” etc. Those skilled in the art willrecognize that “configured to” can generally encompass active-statecomponents and/or inactive-state components and/or standby-statecomponents, unless context requires otherwise.

In addition, even if a specific number of an introduced claim recitationis explicitly recited, those skilled in the art will recognize that suchrecitation should typically be interpreted to mean at least the recitednumber (e.g., the bare recitation of “two recitations,” without othermodifiers, typically means at least two recitations, or two or morerecitations). Furthermore, in those instances where a conventionanalogous to “at least one of A, B, and C, etc.” is used, in generalsuch a construction is intended in the sense one having skill in the artwould understand the convention (e.g., “a system having at least one ofA, B, and C” would include but not be limited to systems that have Aalone, B alone, C alone, A and B together, A and C together, B and Ctogether, and/or A, B, and C together, etc.). In those instances where aconvention analogous to “at least one of A, B, or C, etc.” is used, ingeneral such a construction is intended in the sense one having skill inthe art would understand the convention (e.g., “a system having at leastone of A, B, or C” would include but not be limited to systems that haveA alone, B alone, C alone, A and B together, A and C together, B and Ctogether, and/or A, B, and C together, etc.). It will be furtherunderstood by those within the art that typically a disjunctive wordand/or phrase presenting two or more alternative terms, whether in thedescription, claims, or drawings, should be understood to contemplatethe possibilities of including one of the terms, either of the terms, orboth terms unless context dictates otherwise. For example, the phrase “Aor B” will be typically understood to include the possibilities of “A”or “B” or “A and B.”

With respect to the appended claims, those skilled in the art willappreciate that recited operations therein may generally be performed inany order. Also, although various operational flow diagrams arepresented in a sequence(s), it should be understood that the variousoperations may be performed in other orders than those which areillustrated, or may be performed concurrently. Examples of suchalternate orderings may include overlapping, interleaved, interrupted,reordered, incremental, preparatory, supplemental, simultaneous,reverse, or other variant orderings, unless context dictates otherwise.Furthermore, terms like “responsive to,” “related to,” or otherpast-tense adjectives are generally not intended to exclude suchvariants, unless context dictates otherwise.

It is worthy to note that any reference to “one aspect,” “an aspect,”“an exemplification,” “one exemplification,” and the like means that aparticular feature, structure, or characteristic described in connectionwith the aspect is included in at least one aspect. Thus, appearances ofthe phrases “in one aspect,” “in an aspect,” “in an exemplification,”and “in one exemplification” in various places throughout thespecification are not necessarily all referring to the same aspect.Furthermore, the particular features, structures or characteristics maybe combined in any suitable manner in one or more aspects.

As discussed above, the surgical instruments disclosed herein maycomprise control systems. Each of the control systems can comprise acircuit board having one or more processors and/or memory devices. Amongother things, the control systems are configured to store sensor data,for example. They are also configured to store data which identifies thetype of staple cartridge attached to a stapling instrument, for example.More specifically, the type of staple cartridge can be identified whenattached to the stapling instrument by the sensors and the sensor datacan be stored in the control system. This information can be obtained bythe control system to assess whether or not the staple cartridge issuitable for use.

The surgical instrument systems described herein are motivated by anelectric motor; however, the surgical instrument systems describedherein can be motivated in any suitable manner. In certain instances,the motors disclosed herein may comprise a portion or portions of arobotically controlled system. U.S. patent application Ser. No.13/118,241, entitled SURGICAL STAPLING INSTRUMENTS WITH ROTATABLE STAPLEDEPLOYMENT ARRANGEMENTS, now U.S. Pat. No. 9,072,535, for example,discloses several examples of a robotic surgical instrument system ingreater detail, the entire disclosure of which is incorporated byreference herein. The disclosures of International Patent PublicationNo. WO 2017/083125, entitled STAPLER WITH COMPOSITE CARDAN AND SCREWDRIVE, published May 18, 2017, International Patent Publication No. WO2017/083126, entitled STAPLE PUSHER WITH LOST MOTION BETWEEN RAMPS,published May 18, 2017, International Patent Publication No. WO2015/153642, entitled SURGICAL INSTRUMENT WITH SHIFTABLE TRANSMISSION,published Oct. 8, 2015, U.S. Patent Application Publication No.2017/0265954, filed Mar. 17, 2017, entitled STAPLER WITH CABLE-DRIVENADVANCEABLE CLAMPING ELEMENT AND DUAL DISTAL PULLEYS, U.S. PatentApplication Publication No. 2017/0265865, filed Feb. 15, 2017, entitledSTAPLER WITH CABLE-DRIVEN ADVANCEABLE CLAMPING ELEMENT AND DISTALPULLEY, and U.S. Patent Publication No. 2017/0290586, entitled STAPLINGCARTRIDGE, filed on Mar. 29, 2017, are incorporated herein by referencein their entireties.

EXAMPLE SET 1

Example 1—A surgical instrument system, comprising a surgical instrumentassembly, comprising a shaft, an end effector attached to the shaft, andat least one drive component positioned with the shaft. The surgicalinstrument system further comprises a surgical control circuitcomprising a motor control program configured to run a motor configuredto drive at least one drive component positioned within the shaft. Thesurgical control circuit is configured to receive a first measurement ofa parameter of the motor, and receive a second measurement of aparameter of at least one drive component, wherein the secondmeasurement is sensed locally within the shaft. The surgical controlcircuit is further configured to compare the first measurement and thesecond measurement, determine an actual relationship of the firstmeasurement and the second measurement based on the comparison, comparethe actual relationship to an expected relationship, and adjust themotor control program based on the comparison of the actual relationshipand the expected relationship to align the actual relationship with theexpected relationship.

Example 2—The surgical instrument system of Example 1, wherein theparameter of the motor comprises a parameter of an output shaft attachedto the motor.

Example 3—The surgical instrument system of Examples 1 or 2, wherein theexpected relationship is learned by the surgical control circuit throughthe surgical instrument assembly.

Example 4—The surgical instrument system of Examples 1, 2, or 3, whereinthe second measurement is provided by a linear motion-detecting sensor.

Example 5—The surgical instrument system of Examples 1, 2, 3, or 4,wherein the first measurement is provided by a rotary motion-detectingsensor.

Example 6—The surgical instrument system of Examples 1, 2, 3, 4, or 5,wherein the parameter of the motor comprises dynamic braking of themotor during an intermediate phase of a firing stroke.

Example 7—The surgical instrument system of Examples 1, 2, 3, 4, 5, or6, wherein the parameter of the motor comprises dynamic acceleration ofthe motor during an initial phase of a firing stroke.

Example 8—The surgical instrument system of Examples 1, 2, 3, 4, 5, 6,or 7, wherein the adjustment of the motor control program comprisesrecalibrating the motor control program based on the actualrelationship.

Example 9—A surgical instrument system, comprising a surgical instrumentassembly, comprising a shaft, an end effector attached to the shaft,wherein the end effector comprises a first jaw movable relative to thesecond jaw, and a closure member configured to move the first jawrelative to the second jaw. The surgical instrument system furthercomprises a surgical control circuit comprising a motor control programconfigured to run a motor configured to actuate the closure member. Thesurgical control circuit is configured to determine when the motorrotates a first amount corresponding to a first expected displacement ofthe closure member with a motor encoder, determine an actualdisplacement of the closure member with a sensor positioned within theshaft, compare the actual displacement of the closure member and thefirst expected displacement of the closure member, determine anadditional target displacement corresponding to a second expecteddisplacement of the closure member; and recalibrate the motor controlprogram to rotate the motor sufficient to drive the closure member thesecond expected displacement.

Example 10—A surgical instrument assembly, comprising a shaft, an endeffector attached to the shaft, a firing member configured to movethrough the end effector during a firing stroke, and a stretchableoptical waveguide attached to the shaft and the firing member, whereinthe stretchable optical waveguide is configured to stretch as the firingmember is moved through the firing stroke. The surgical instrumentassembly further comprises a light sensor configured to sense a changein light presence within the stretchable optical waveguide during thefiring stroke, and a control circuit configured to monitor signalsreceived from the light sensor to determine at least one parameter ofthe firing member during the firing stroke.

Example 11—The surgical instrument assembly of Example 10, furthercomprising an articulation joint attaching the end effector to theshaft, wherein the stretchable optical waveguide is attached to theshaft proximal to the articulation joint.

Example 12—The surgical instrument assembly of Examples 10 or 11,wherein the stretchable optical waveguide comprises one or morevertical-cavity surface-emitting lasers and one or more photo diodes.

Example 13—The surgical instrument assembly of Example 12, wherein thephoto diode is configured to measure a loss of light in the stretchableoptical waveguide as the waveguide is stretched during the firingstroke.

Example 14—A surgical instrument assembly, comprising a shaft, an endeffector attached to the shaft, and a firing member configured to movethrough the end effector during a firing stroke, wherein the firingmember comprises a plurality of windows defined in the firing member.The surgical instrument assembly further comprises a light source, and alight sensor configured to detect the light source, wherein theplurality of windows are configured to pass between the light source andthe light sensor as the firing member moves through the firing stroke.The surgical instrument assembly further comprises a control circuitconfigured to monitor signals received from the light sensor todetermine at least one parameter of the firing member during the firingstroke.

Example 15—The surgical instrument assembly of Example 14, wherein theplurality of windows comprise a pattern corresponding to linear distancetraveled by the firing member.

Example 16—A surgical instrument assembly, comprising a shaft, an endeffector attached to the shaft, a firing member configured to movethrough the end effector during a firing stroke, and a sensing circuitcomprising a stretchable resistive cable attached to the shaft and thefiring member, wherein the stretchable resistive cable is configured tostretch as the firing member is moved through the firing stroke. Thesurgical instrument assembly further comprises a control circuitconfigured to monitor the resistance of the sensing circuit to determineat least one parameter of the firing member during the firing stroke.

Example 17—A surgical instrument system, comprising a surgicalinstrument assembly that comprises a shaft, an end effector attached tothe shaft, and a firing member configured to move through the endeffector during a firing stroke, wherein the firing member comprises amagnet. The surgical instrument system further comprises a first Halleffect sensor positioned at a beginning of the firing stroke, and asecond Hall effect sensor positioned at an end of the firing stroke. Thesurgical instrument system further comprises a surgical control circuit,comprising a motor, and a control circuit comprising a motor controlprogram. The control circuit is configured to monitor the rotation ofthe motor, compare the rotation of the motor to signals received fromthe first Hall effect sensor and the second Hall effect sensor,determine if the firing member has moved an expected distance based onthe comparison of the rotation of the motor and the signals receivedfrom the first Hall effect sensor and the second Hall effect sensor, andrecalibrate the motor control program if the firing member has not movedthe expected distance. The surgical instrument system further comprisesa sensing circuit comprising a stretchable resistive cable attached tothe shaft and the firing member, wherein the stretchable resistive cableis configured to stretch as the firing member is moved through thefiring stroke. The surgical instrument system further comprises acontrol circuit configured to monitor the resistance of the sensingcircuit to determine at least one parameter of the firing member duringthe firing stroke.

Example 18—A surgical instrument, comprising a shaft, an end effectorattached to the shaft, and a firing system comprising an electric motorand a firing member configured to move through the end effector during afiring stroke. The surgical instrument further comprises a stretchableoptical waveguide attached to the shaft and the firing member, whereinthe stretchable optical waveguide is configured to stretch as the firingmember is moved through the firing stroke. The surgical instrumentfurther comprises a light sensor configured to sense a change in lightpresence within the stretchable optical waveguide during the firingstroke, an encoder configured to evaluate the rotation of the electricmotor, and a control circuit. The control circuit is configured tomonitor signals received from the light sensor and the encoder todetermine distortions in the firing member that cause the motion of thefiring member to depart from an expected motion.

Example 19—The surgical instrument of Example 18, further comprising anarticulation joint attaching the end effector to the shaft, wherein thestretchable optical waveguide is attached to the shaft proximal to thearticulation joint, wherein the firing member extends through thearticulation joint, and wherein the distortions in the firing memberarise from the articulation of the end effector.

Example 20—A surgical instrument, comprising a shaft, an end effectorattached to the shaft, a firing member configured to move through theend effector during a firing stroke, wherein the firing member comprisesa plurality of windows defined in the firing member. The surgicalinstrument further comprises an electric motor configured to drive thefiring member, a light source, and a light sensor configured to detectthe light source, wherein the plurality of windows are configured topass between the light source and the light sensor as the firing membermoves through the firing stroke. The surgical instrument furthercomprises an encoder configured to evaluate the rotation of the electricmotor, and a control circuit configured to monitor signals received fromthe light sensor and the encoder to determine distortions in the firingmember that cause the motion of the firing member to depart from anexpected motion.

Example 21—The surgical instrument of Example 20, further comprising anarticulation joint attaching the end effector to the shaft, wherein thefiring member extends through the articulation joint, and wherein thedistortions in the firing member arise from the articulation of the endeffector.

Example 22—A surgical instrument, comprising a shaft, an end effectorattached to the shaft, and a firing member configured to move throughthe end effector during a firing stroke, wherein the firing membercomprises a first band and a second band. The surgical instrumentfurther comprises a sensing circuit comprising a first stretchableresistive cable attached to the shaft and the first band and a secondstretchable resistive cable attached to the shaft and the second band,wherein the first stretchable resistive cable and the second stretchableresistive cable are configured to stretch as the firing member is movedthrough the firing stroke. The surgical instrument further comprises acontrol circuit configured to monitor the resistance of the sensingcircuit to determine at least one parameter of the firing member duringthe firing stroke.

Example 23—The surgical instrument of Example 22, further comprising anarticulation joint attaching the end effector to the shaft, wherein thefiring member extends through the articulation joint, and whereindistortions in the firing member arise from the articulation of the endeffector that are detectable by the control circuit.

EXAMPLE SET 2

Example 1—A surgical instrument assembly, comprising a shaft, anarticulation joint, and an end effector attached to the shaft by way ofthe articulation joint, wherein the end effector is configured to bearticulated about the articulation joint. The surgical instrumentassembly further comprises a flex circuit extending through the shaftand connected to the end effector, wherein the flex circuit comprises anarticulation section aligned with the articulation joint. Thearticulation section comprises a predefined bend profile configured tostretch across the articulation joint predictably as the end effector isarticulated about the articulation joint.

Example 2—The surgical instrument assembly of Example 1, wherein thearticulation section comprises elastic connection members configured tobias the articulation section into the predefined bend profile.

Example 3—A surgical instrument assembly, comprising a shaft, anarticulation joint, an end effector attached to the shaft by way of thearticulation joint, and a flex circuit extending through the shaft. Theflex circuit comprises a non-flexible zone, and a flexible zoneextending across the articulation joint.

Example 4—The surgical instrument assembly of Example 3, wherein theflex circuit further comprises conductible flexible inks and conductiblemetallic traces.

Example 5—A surgical instrument assembly, comprising a shaft, anarticulation joint, an end effector attached to the shaft by way of thearticulation joint, and a flex circuit extending through the shaft. Theflex circuit comprises a flexible section configured to be stretched ina predetermined direction. The flexible section comprises a relaxedstate, a stretched state, and a plurality of elastic connection membersattached to the flex circuit within the flexible section. The pluralityof elastic connection members are configured to bias the flexiblesection into the relaxed state and permit the stretching of the flexiblesection in the predetermined direction.

Example 6—The surgical instrument assembly of Example 5, wherein theelastic connection members are oriented along the predetermineddirection.

Example 7—A surgical instrument assembly, comprising a shaft, an endeffector attached to the shaft, and a flex circuit extending through theshaft. The flex circuit comprises a flex circuit profile plane, and apre-curved section where the flex circuit is bent such that the flexcircuit profile plane is aligned in a single plane throughout thepre-curved section.

Example 8—The surgical instrument assembly of Example 7, furthercomprising an articulation joint, wherein the pre-curved section extendsacross the articulation joint, and wherein the pre-curved section ispositioned off-center with respect to a central shaft axis defined bythe shaft.

Example 9—A surgical instrument assembly, comprising a shaft, an endeffector attached to the shaft, and a flex circuit extending through theshaft. The flex circuit comprises a flex circuit profile plane, and apre-bent section where the flex circuit is bent such that the flexcircuit profile plane is not aligned in a single plane throughout thepre-bent section.

Example 10—The surgical instrument assembly of Example 9, furthercomprising an articulation joint, wherein the pre-bent section extendsacross the articulation joint, and wherein the pre-bent section ispositioned off-center with respect to a central shaft axis defined bythe shaft.

Example 11—A surgical instrument assembly, comprising a shaft, an endeffector, and a wiring harness extending through the shaft. The wiringharness comprises at least one first zone comprising a non-stretchableportion, and a second zone comprising a stretchable portioninterconnecting the at least one first zone.

Example 12—The surgical instrument assembly of Example 11, wherein thefirst zone comprises a bendable portion.

Example 13—The surgical instrument assembly of Examples 11 or 12,wherein the stretchable portion comprises conductive ink.

Example 14—The surgical instrument assembly of Examples 11, 12, or 13,wherein the stretchable zone comprises metallic traces.

Example 15—The surgical instrument assembly of Examples 11, 12, 13, or14, further comprising drive components positioned within the shaft,wherein the wiring harness is attached to at least one of the drivecomponents in at least one location of the at least one of the drivecomponents.

Example 16—The surgical instrument assembly of Example 15, wherein theat least one location comprises an index location, and wherein the indexlocation defines a reference for at least one sensor of the wiringharness.

Example 17—The surgical instrument assembly of Example 16, wherein theat least one sensor is configured to monitor a parameter of the at leastone of the drive components.

Example 18—A surgical instrument, comprising a shaft defining alongitudinal axis, an end effector, and an articulation joint, whereinthe end effector is rotatably attached to the shaft about thearticulation joint. The surgical instrument further comprises anarticulation driver mounted to the end effector, wherein thearticulation driver is translatable longitudinally to rotate the endeffector about the articulation joint. The surgical instrument furthercomprises a wiring harness. The wiring harness comprises a shaft portionextending within the shaft, an end effector portion extending within theend effector, and an anchor portion mounted to the articulation driver.The wiring harness further comprises a first flexible bend extendingbetween the shaft portion and the anchor portion, and a second flexiblebend extending between the anchor portion and the end effector portion.

Example 19—The surgical instrument of Example 18, wherein the wiringharness comprises a first biasing member configured to return the firstflexible bend to an unflexed state.

Example 20—The surgical instrument of Example 19, wherein the wiringharness comprises a second biasing member configured to return thesecond flexible band to an unflexed state.

Example 21—The surgical instrument of Examples 18, 19, or 20, whereinthe wiring harness comprises a flex circuit comprised of polyimidelayers.

Example 22—The surgical instrument of Example 21, wherein the wiringharness further comprises metallic electrical traces on the polyimidelayers.

Example 23—The surgical instrument of Example 22, wherein the metallicelectrical traces are comprised of metallic ink.

Example 24—The surgical instrument of Examples 18, 19, 20, 21, 22, or,23, wherein the wiring harness further comprises silicone regionsconfigured to permit the wiring harness to stretch.

Example 25—The surgical instrument of Example 24, wherein the metallicelectrical traces extend over the silicone regions.

Example 26—The surgical instrument of Example 25, wherein the metallicelectrical traces follow arcuate paths across the silicone regions.

Example 27—The surgical instrument of Examples 22, 23, 24, 25, or 26,wherein the metallic electrical traces are comprised of conductive ink.

Example 28—The surgical instrument of Examples 21, 22, 23, 24, 25, 26,or 27, wherein the wiring harness further comprises an aperture definedin the flex circuit and a printed circuit board positioned in theaperture, and wherein the printed circuit board is in communication withelectrical traces in the flex circuit.

Example 29—A surgical instrument, comprising a shaft defining alongitudinal axis, an end effector, and an articulation joint, whereinthe end effector is rotatably attached to the shaft about thearticulation joint. The surgical instrument further comprises a flexcircuit. The flex circuit comprises a shaft portion extending within theshaft, and an end effector portion extending within the end effector.

Example 30—The surgical instrument of Example 29, wherein the flexcircuit is comprised of polyimide layers.

Example 31—The surgical instrument of Example 30, wherein the flexcircuit further comprises metallic electrical traces on the polyimidelayers.

Example 32—The surgical instrument of Example 31, wherein the metallicelectrical traces are comprised of metallic ink.

Example 33—The surgical instrument of Examples 29, 30, 31, or 32,wherein the flex circuit further comprises silicone regions configuredto permit the wiring harness to stretch.

Example 34—The surgical instrument of Example 33, wherein the metallicelectrical traces extend over the silicone regions.

Example 35—The surgical instrument of Examples 33 or 34, wherein themetallic electrical traces follow arcuate paths across the siliconeregions.

Example 36—The surgical instrument of Examples 31, 32, 33, 34, 35, or36, wherein the metallic electrical traces are comprised of conductiveink.

Example 37—The surgical instrument of Examples 29, 30, 31, 32, 33, 34,35, or 36, wherein the flex circuit further comprises an aperturedefined therein and a printed circuit board positioned in the aperture,and wherein the printed circuit board is in communication withelectrical traces in the flex circuit.

Example 38—The surgical instrument of Example 37, wherein the printedcircuit board is comprised of fiberglass.

Example 39—The surgical instrument of Examples 29, 30, 31, 32, 33, 34,35, 36, 37, or 38, wherein the flex circuit further comprises anaperture defined therein and a microchip positioned in the aperture, andwherein the microchip is in communication with electrical traces in theflex circuit.

EXAMPLE SET 3

Example 1—A surgical instrument assembly, comprising a shaft, and an endeffector extending from the shaft. The end effector comprises a firstjaw, a second jaw movable relative to the first jaw, and an anvil. Theend effector further comprises a staple cartridge channel, a staplecartridge positioned within the staple cartridge channel, and aplurality of pressure sensors positioned between the staple cartridgeand the staple cartridge channel configured to detect clamping pressurewithin the end effector.

Example 2—The surgical instrument assembly of Example 1, wherein the endeffector comprises a first side and a second side defined by a firingstroke path, and wherein the plurality of pressure sensors arepositioned on both the first side and the second side.

Example 3—The surgical instrument assembly of Examples 1 or 2, whereinthe plurality of pressure sensors are distributed longitudinally along afiring stroke path.

Example 4—The surgical instrument assembly of Examples 1, 2, or 3,further comprising a flex circuit coupled to the plurality of pressuresensors.

Example 5—A surgical instrument assembly, comprising a shaft, and adrive member movable within the shaft, wherein the drive membercomprises a discontinuity portion. The surgical instrument assemblyfurther comprises a flex circuit positioned within shaft and coupled toa surgical control circuit. The flex circuit comprises an integratedstrain gauge mounted on the drive member within the discontinuityportion, wherein the surgical control circuit is configured to determinea load experienced by the drive member by way of the strain gauge.

Example 6—The surgical instrument assembly of Example 5, wherein thediscontinuity portion comprises a necked-down portion.

Example 7—The surgical instrument assembly of Examples 5 or 6, whereinthe drive member comprises a channel spine comprising a channelpositioned on a distal end of the drive member, wherein the channel isconfigured to receive a staple cartridge therein.

Example 8—The surgical instrument assembly of Examples 5, 6, or 7,wherein the drive member comprises a first drive member, wherein thesurgical instrument assembly further comprises a second drive membermovable within the shaft, wherein the integrated strain gauge comprisesa first integrated strain gauge, and wherein the flex circuit furthercomprises a second integrated strain gauge mounted on the second drivemember.

Example 9—The surgical instrument assembly of Examples 5, 6, 7, or 8,wherein the flex circuit comprises a flexible portion and a non-flexibleportion.

Example 10—The surgical instrument assembly of Examples 5, 6, 7, 8, or9, wherein the drive member further comprises a primary body portion,and wherein the discontinuity portion is configured to experience morestrain than the primary body portion.

Example 11—A surgical instrument system, comprising: a batch of staplecartridges, wherein each staple cartridge of the batch of staplecartridges comprises a predetermined load profile range. The surgicalinstrument system further comprises a surgical instrument assembly,wherein a staple cartridge of the batch of staple cartridges isconfigured to be installed into the surgical instrument assembly. Thesurgical instrument system further comprises a control circuit. Thecontrol circuit is configured to detect the predetermined load profilerange of the installed staple cartridge, execute a motor control programto fire the installed staple cartridge with the surgical instrumentassembly, and monitor an actual load profile of the installed staplecartridge when the installed staple cartridge is fired. The controlcircuit is further configured to compare the predetermined load profilerange and the actual load profile, output the result of the comparisonof the predetermined load profile range and the actual load profile, andmodify the motor control program such that each subsequent staplecartridge of the batch of staple cartridges installed into the surgicalinstrument assembly is fired within the predetermined load profilerange.

Example 12—A surgical instrument assembly, comprising a shaft, an endeffector attached to the shaft, and a sub-component system configured toexperience strain within the surgical instrument assembly. The surgicalinstrument assembly further comprises a woven conductive fabric attachedto the sub-component system. The woven conductive fabric comprises aprimary body portion, and a plurality of conductive fibers extendingthrough the primary body portion. The surgical instrument assemblyfurther comprises a control circuit configured to monitor the resistanceof the woven conductive fabric and determine the load on thesub-component based on the resistance of the woven conductive fabric.

Example 13—The surgical instrument assembly of Example 12, wherein theplurality of conductive fibers are woven.

Example 14—The surgical instrument assembly of Examples 12 or 13,wherein the plurality of conductive fibers are wired in parallel.

Example 15—The surgical instrument assembly of Examples 12 or 13,wherein the plurality of conductive fibers are wired in series.

Example 16—The surgical instrument assembly of Examples 12, 13, 14, or15, wherein the woven conductive fabric is attached to a groundedlocation within the shaft.

Example 17—The surgical instrument assembly of Examples 12, 13, 14, 15,or 16, wherein the woven conductive fabric comprises a first wovenconductive fabric, wherein the first woven conductive fabric isconfigured to measure load applied to the sub-component system in afirst plane, wherein the surgical instrument assembly further comprisesa second woven conductive fabric configured to measure load applied tothe sub-component system in a second plane.

Example 18—The surgical instrument assembly of Example 12, wherein theresistance of the woven conductive fabric is configured to correspond todisplacement of the sub-component system.

Example 19—A surgical instrument assembly, comprising a shaft, anarticulation joint, and an end effector attached to the shaft by way ofthe articulation joint. The surgical instrument assembly furthercomprises a firing member comprising a plurality of bands attached toeach other, and a plurality of conductive fabrics, wherein each the bandcomprises the conductive fabric attached thereto. The surgicalinstrument assembly further comprises a control circuit configured tomonitor the resistance of each conductive fabric to measure a parameterof each band.

Example 20—The surgical instrument assembly of Example 19, wherein eachconductive fabric comprises a plurality of conductive fibers.

Example 21—The surgical instrument assembly of Example 19, wherein eachconductive fabric comprises a single conductive fiber.

Example 22—The surgical instrument assembly of Examples 19, 20, or 21,wherein each band comprises an electrical contact positioned on aproximal end thereof.

Example 23—The surgical instrument assembly of Examples 19, 20, 21, 22,or 23, wherein the plurality of conductive fabrics comprises a pluralityof conductive textiles.

Example 24—The surgical instrument assembly of Examples 19, 20, 21, 22,23, or 24, wherein the plurality of conductive fabrics comprises aplurality of metalized conductive fabrics.

Example 25—A surgical instrument assembly, comprising a shaft, an endeffector attached to the shaft, and an actuation member movable withinthe shaft, wherein the actuation member comprises a partially opaqueportion. The surgical instrument assembly further comprises a sensingsystem configured to detect a load on the actuation member. The sensingsystem comprises a light source directed toward the partially opaqueportion of the actuation member, and a sensor configured to detectresultant light diffraction caused by the partially opaque portion ofthe actuation member. The resultant light diffraction comprises a rangeof diffraction patterns corresponding to the load on the actuationmember.

Example 26—A surgical instrument assembly, comprising a shaft comprisinga first distal end, an articulation joint comprising a distal-mostarticulation link, and an end effector attached to the shaft by way ofthe articulation joint, wherein the end effector is coupled to thedistal-most articulation link. The surgical instrument assembly furthercomprises an articulation drive member configured to articulate the endeffector about the articulation joint, wherein the articulation drivemember is movable relative to the shaft, and wherein the articulationdrive member comprises a second distal end. The surgical instrumentassembly further comprises a Hall effect sensor attached to the seconddistal end of the articulation joint, a magnet attached to thedistal-most articulation link, wherein the distal-most articulation linkis actuatable to a fully-articulated position. The surgical instrumentassembly further comprises a surgical control circuit configured tomonitor the position of the magnet by way of the Hall effect sensor, andadvance the articulation drive member to move the distal-mostarticulation link to the fully-articulated position based on theposition of the magnet.

Example 27—A surgical instrument assembly, comprising a shaft comprisinga first distal end, an articulation joint comprising a distal-mostarticulation link, and an end effector attached to the shaft by way ofthe articulation joint, wherein the end effector is coupled to thedistal-most articulation link. The surgical instrument assembly furthercomprises an articulation drive member configured to articulate the endeffector about the articulation joint, wherein the articulation drivemember is movable relative to the shaft, and wherein the articulationdrive member comprises a second distal end. The surgical instrumentassembly further comprises a Hall effect sensor attached to the seconddistal end of the articulation joint, a magnet attached to thedistal-most articulation link, wherein the distal-most articulation linkis actuatable to a fully-articulated position. The surgical instrumentassembly further comprises a surgical control circuit configured tomonitor a dynamic parameter of the magnet by way of the Hall effectsensor, and advance the articulation drive member to move thedistal-most articulation link to the fully-articulated position based onthe monitored dynamic parameter of the magnet.

Example 28—A surgical instrument, comprising a shaft comprising a frame,wherein the frame comprises a discontinuity portion. The surgicalinstrument further comprises a drive member movable within the shaft,and a flex circuit positioned within shaft and coupled to a controlcircuit. The flex circuit comprises an integrated strain gauge mountedon the frame within the discontinuity portion, wherein the controlcircuit is configured to determine a load experienced by the shaft byway of the strain gauge.

Example 29—The surgical instrument of Example 28, wherein thediscontinuity portion comprises a notch, wherein the notch comprises adepth, wherein the integrated strain gauge comprises a thickness, andwherein the thickness does not exceed the depth.

Example 30—The surgical instrument of Examples 28 or 29, wherein theflex circuit comprises a longitudinal portion and the integrated straingauge comprises a tab extending laterally from the longitudinal portion.

Example 31—The surgical instrument of Example 30, wherein thelongitudinal portion is flexible and the tab is rigid.

Example 32—The surgical instrument of Examples 30 or 31, wherein thelongitudinal portion is not mounted to the frame.

Example 33—The surgical instrument of Examples 30, 31, or 32, whereinthe tab is mounted to the frame by at least one adhesive.

Example 34—The surgical instrument of Examples 28, 29, 30, 31, 32, or33, wherein the discontinuity comprises a necked-down portion comprisinga smaller cross-section than a distal frame portion positioned distallywith respect to the necked-down portion and a proximal frame portionpositioned proximally with respect to the necked-down portion.

Example 35—The surgical instrument of Examples 28, 29, 30, 31, 32, 33,or 34, wherein the discontinuity comprises a fin extending outwardlytherefrom, and wherein the integrated strain gauge is mounted to thefin,

Example 36—A surgical instrument, comprising a shaft comprising a frame,a drive member movable within the shaft, and a flex circuit positionedwithin shaft and coupled to a control circuit. The flex circuitcomprises connector portions and flexible portions, wherein theconnector portions connect the flexible portions, wherein the flexibleportions comprise integrated strain gauges mounted to the frame, andwherein the connector portions comprise signal circuits in communicationwith the integrated strain gauges.

Example 37—The surgical instrument of Example 36, wherein the connectorportions of the flex circuit comprises a plurality of attached layers,and wherein the flexible portions comprise less layers than theconnector portions.

Example 38—A surgical instrument, comprising a shaft, a sub-componentsystem configured to experience strain within the surgical instrumentassembly, and a woven conductive fabric attached to the sub-componentsystem. The woven conductive fabric comprises a body portion, and aplurality of conductive fibers extending through the body portion. Thesurgical instrument further comprises a control circuit configured tomonitor the resistance of the woven conductive fabric and determine theload on the sub-component based on the resistance of the wovenconductive fabric.

Example 39—The surgical instrument of Example 38, wherein the pluralityof conductive fibers comprises a first portion in which the conductivefibers are oriented in a first direction and a second portion in whichthe conductive fibers are oriented in a second direction which isdifferent than the first direction.

Example 40—The surgical instrument of Example 39, wherein the firstdirection is orthogonal to the second direction.

Example 41—The surgical instrument of Examples 38, 39, or 40, whereinthe plurality of conductive fibers comprises a first portion attached toa first region of the sub-component system and a second portion attachedto a second region of the sub-component system which is different thanthe first region.

Example 42—The surgical instrument of Example 41, wherein the firstregion is stiffer than the second region, wherein the first portion isused to measure a force in the sub-component system, and wherein thesecond portion is used to measure a strain in the subcomponent system.

Example 43—The surgical instrument of Examples 38, 39, 40, 41, or 42,wherein the plurality of conductive fibers comprises a first portionattached to a first sub-component of the sub-component system and asecond portion attached to a second sub-component of the sub-componentsystem which is different than the first sub-component.

Example 44—The surgical instrument of Example 43, wherein the firstsub-component comprises a first layer of a firing member and the secondsub-component comprises a second layer of the firing member.

EXAMPLE SET 4

Example 1—A surgical instrument assembly, comprising a frame, anactuation member configured to be actuated through an actuation strokewithin the frame, and a flex circuit extending through the frame. Theflex circuit is configured to be commutatively coupled with a surgicalcontrol circuit, and wherein the flex circuit comprises an integratedsensor configured to detect a parameter of the actuation member.

Example 2—The surgical instrument assembly of Example 1, wherein theintegrated sensor comprises a Hall effect sensor, and wherein theactuation member comprises a magnet positioned on the actuation member.

Example 3—The surgical instrument assembly of Examples 1 or 2, whereinthe parameter comprises displacement of the actuation member.

Example 4—The surgical instrument assembly of Examples 1, 2, or 3,wherein the parameter comprises velocity of the actuation member.

Example 5—The surgical instrument assembly of Examples 1, 2, 3, or 4,wherein the parameter comprises acceleration of the actuation member.

Example 6—The surgical instrument assembly of Examples 1, 2, 3, 4, or 5,wherein the actuation member comprises a firing member.

Example 7—The surgical instrument assembly of Examples 1, 2, 3, 4, 5, or6, wherein the actuation member comprises a closure member.

Example 8—The surgical instrument assembly of Examples 1, 2, 3, 4, 5, 6,or 7, wherein the actuation member comprises an articulation member.

Example 9—The surgical instrument assembly of Examples 1, 3, 4, 5, 6, 7,or 8, wherein the integrated sensor comprises a Hall effect sensor,wherein the actuation member comprises a plurality of magnets positionedon the actuation member, wherein a first magnet of the plurality ofmagnets is oriented in an inverted polar relationship to a second magnetof the plurality of magnets, wherein the Hall effect sensor isconfigured to sense both magnets simultaneously.

Example 10—The surgical instrument assembly of Examples 1, 2, 3, 4, 5,6, 7, 8, or 9, wherein the actuation member comprises a rotary drivemember.

Example 11—The surgical instrument assembly of Examples 1, 2, 3, 4, 5,6, 7, 8, 9, or 10, wherein the actuation member comprises a rotary drivemember, wherein the rotary drive member comprises alternating magnetspositioned on the rotary drive member, and wherein the surgicalinstrument assembly further comprises a coil configured to alter amagnetic field.

Example 12—The surgical instrument assembly of Examples 1, 2, 3, 4, 5,6, 7, 8, 9, 10, or 11, wherein the actuation member comprises a closuremember, wherein the integrated sensor comprises a Hall effect sensor,wherein the closure member comprises a first magnet arranged at a firstpolarity relative to the Hall effect sensor and a second magnet arrangedat a second polarity relative to the Hall effect sensor.

Example 13—The surgical instrument assembly of Examples 1, 2, 3, 4, 5,6, 7, 8, 9, 10, 11, or 12, further comprising an end effector,comprising a first jaw, and a second jaw movable relative to the firstjaw to clamp tissue. The actuation member comprises a closure memberconfigured to move the second jaw relative to the first jaw, and whereinthe parameter comprises displacement of the closure member to determinethe position of the second jaw relative to the first jaw.

Example 14—The surgical instrument assembly of Examples 1, 2, 3, 4, 5,6, 7, 8, 9, 10, 11, 12, or 13, wherein the actuation member comprises aplurality of magnets positioned on the actuation member, wherein theintegrated sensor comprises a Hall effect sensor, and wherein the Halleffect sensor is configured to sense the plurality of magnets during theactuation stroke.

Example 15—The surgical instrument assembly of Example 14, wherein theplurality of magnets comprise a beginning-of-stroke magnet and anend-of-stroke magnet each arranged at a polarity relative to the Halleffect sensor that is opposite to a polarity at which all of the othermagnets of the plurality of magnets are arranged.

Example 16—The surgical instrument assembly of Examples 1, 2, 3, 4, 5,6, 7, 8, 9, 10, 11, 12, 13, 14, or 15, wherein the integrated sensorcomprises a capacitive sensor.

Example 17—The surgical instrument assembly of Examples 1, 2, 3, 4, 5,6, 7, 8, 9, 10, 11, 12, 13, 14, 15, or 16, wherein the integrated sensorcomprises an optical sensor.

Example 18—A surgical instrument, comprising a housing, a shaftextending from the housing, an end effector extending from the shaft, adrive system, and a flexible circuit assembly extending within theshaft. The flexible circuit assembly comprises a power transmissionbackbone and a signal communication backbone, and wherein the signalcommunication backbone is separated from the power transmissionbackbone.

Example 19—The surgical instrument of Example 18, wherein thecommunication backbone comprises communication circuits in communicationwith a multiplexer.

Example 20—The surgical instrument of Examples 18 or 19, wherein theflexible circuit assembly comprises a first region, and a second region,wherein the first region and the second region are different. Theflexible circuit assembly further comprises a first circuit incommunication with the first region, a second circuit in communicationwith the second region, and a voltage control circuit configured tolimit the voltage to the first region while providing a differentvoltage to the second region.

Example 21—The surgical instrument of Example 20, wherein the firstregion comprises a first sensor in communication with the first circuit,and wherein the second region comprises a second sensor in communicationwith the second circuit.

Example 22—The surgical instrument of Example 21, wherein the firstsensor is configured to detect a first component of the drive system andthe second sensor is configured to detect a second component of thedrive system.

Example 23—The surgical instrument of Examples 20, 21, or 22, whereinthe voltage provided to the first region is 6 volts and the voltageprovided to the second region is 12 volts.

Example 24—The surgical instrument of Examples 18, 19, 20, 21, 22, or23, wherein the flexible circuit assembly comprises a first region, anda second region, wherein the first region and the second region aredifferent. The flexible circuit assembly further comprises a firstcircuit in communication with the first region, a second circuit incommunication with the second region, and a controller configured tolimit the quantity of data transmitted via the first circuit during afirst operating mode and to increase the quantity of data transmittedvia the first circuit during a second operating mode.

Example 25—The surgical instrument of Examples 20, 21, 22, 23, or 24,wherein the first region comprises a first sensor in communication withthe first circuit, and wherein the second region comprises a secondsensor in communication with the second circuit.

Example 26—The surgical instrument of Example 25, wherein the firstsensor is configured to detect a first component of the drive system andthe second sensor is configured to detect a second component of thedrive system.

Example 27—A surgical instrument, comprising a housing, a shaftextending from the housing, and an end effector extending from theshaft. The surgical instrument further comprising a drive system; and aflexible circuit assembly extending within the shaft. The flexiblecircuit assembly comprises a first region comprising a first sensorcircuit, wherein the first sensor circuit is configured to generate afirst ping signal in response to a first event. The flexible circuitassembly further comprises a second region comprising a second sensorcircuit, wherein the first region and the second region are different,wherein the second sensor circuit is configured to generate a secondping signal in response to a second event. The flexible circuit assemblyfurther comprises a controller in communication with the first sensorcircuit and the second sensor circuit. The controller holds the firstsensor circuit in a first low power mode until it receives the firstping signal, wherein the controller places the first sensor circuit in afirst high power mode once it receives the first ping signal. Thecontroller holds the second sensor circuit in a second low power modeuntil it receives the second ping signal, and wherein the controllerplaces the second sensor circuit in a second high power mode once itreceives the second ping signal.

Example 28—A surgical instrument, comprising a housing, a shaftextending from the housing, an end effector extending from the shaft, adrive system; and a flexible circuit assembly extending within theshaft. The flexible circuit assembly comprises a first region comprisinga first sensor circuit including a first sensor, and a second regioncomprising a second sensor circuit including a second sensor, whereinthe first region and the second region are different. The flexiblecircuit assembly further comprises a controller in communication withthe first sensor circuit and the second sensor circuit. The first sensorcircuit is in a first low power mode until it receives a first pingsignal from the controller, wherein the first sensor circuit enters intoa first high power mode when it receives the first ping signal. Thesecond sensor circuit is in a second low power mode until it receives asecond ping signal from the controller, and wherein the second sensorcircuit enters into a second high power mode when it receives the secondping signal.

Example 29—A surgical instrument, comprising a housing, a shaftextending from the housing, an end effector extending from the shaft, adrive system, and a flexible circuit assembly extending within theshaft. The flexible circuit assembly comprises a first region comprisinga first sensor circuit, wherein the first sensor circuit is configuredto generate a first ping signal in response to a first event. Theflexible circuit assembly further comprises a second region comprising asecond sensor circuit, wherein the first region and the second regionare different, wherein the second sensor circuit is configured togenerate a second ping signal in response to a second event. Theflexible circuit assembly further comprises a controller incommunication with the first sensor circuit and the second sensorcircuit. The controller holds the first sensor circuit in a first lowdata bandwidth mode until it receives the first ping signal, wherein thecontroller places the first sensor circuit in a first high databandwidth mode once it receives the first ping signal. The controllerholds the second sensor circuit in a second low data bandwidth modeuntil it receives the second ping signal, and wherein the controllerplaces the second sensor circuit in a second high data bandwidth modeonce it receives the second ping signal.

Example 30—A surgical instrument, comprising a housing, a shaftextending from the housing, an end effector extending from the shaft, adrive system, and a flexible circuit assembly extending within theshaft. The flexible circuit assembly comprises a first region comprisinga first sensor circuit including a first sensor, a second regioncomprising a second sensor circuit including a second sensor, whereinthe first region and the second region are different. The flexiblecircuit assembly further comprises a controller in communication withthe first sensor circuit and the second sensor circuit. The first sensorcircuit is in a first low data bandwidth mode until it receives a firstping signal from the controller, wherein the first sensor circuit entersinto a first high data bandwidth mode when it receives the first pingsignal. The second sensor circuit is in a second low data bandwidth modeuntil it receives a second ping signal from the controller, wherein thesecond sensor circuit enters into a second high data bandwidth mode whenit receives the second ping signal.

Example 31—The surgical instrument of Example 30, wherein the drivesystem comprises a drive member, wherein the first sensor and the secondsensor are configured to detect the position of the drive member,wherein the second sensor circuit enters into the second high databandwidth mode when the first sensor circuit detects the movement of thedrive member.

Example 32—The surgical instrument of Examples 30 or 31, wherein thecontroller places the second sensor circuit in the second high databandwidth mode if the controller determines that the total system databandwidth sufficiently exceeds the data bandwidth consumed by the firstsensor circuit.

Example 33—The surgical instrument of Examples 30, 31, or 32, whereinthe controller increases the sampling rate of the second sensor when thesecond sensor circuit is in the second high data bandwidth mode.

Example 34—The surgical instrument of Examples 30, 31, 32, or 33,wherein the controller holds the second sensor circuit in the second lowdata bandwidth mode if the total system data bandwidth does notsufficiently exceed the data bandwidth consumed by the first sensorcircuit.

Example 35—The surgical instrument of Examples 30, 31, 32, 33, or 34,wherein the controller throttles the second sensor circuit into thesecond low data bandwidth mode if the total system data bandwidth doesnot sufficiently exceed the data bandwidth consumed by the first sensorcircuit.

Example 36—The surgical instrument of Examples 30, 31, 32, 33, 34, or35, wherein the controller reduces the sampling rate of the secondsensor to throttle the second sensor circuit into the second low databandwidth mode.

Example 37—The surgical instrument of Examples 30, 31, 32, 33, 34, or35, wherein the controller reduces the bit size of the data transmittedby the second sensor to throttle the second sensor circuit into thesecond low data bandwidth mode.

Example 38—A surgical instrument drive system, comprising an electricmotor, a rotary drive shaft driveable by the electric motor, and a drivemember driveable by the rotary drive shaft. The surgical instrumentdrive system further comprises an array of magnetic elements mounted tothe rotary drive shaft, an array of sensing coils configured to detectthe presence of the array of magnetic elements, and a controller incommunication with the array of sensing coils. The controller isconfigured to assess the position of the drive member by data from thearray of sensing coils.

Example 39—The surgical instrument drive system of Example 38, whereinthe array of magnetic elements comprises a first magnetic elementpositioned on a first side of the rotary drive shaft and a secondmagnetic element positioned on a second side of the rotary drive shaftwhich is opposite the first side.

Example 40—The surgical instrument drive system of Example 39, whereinthe first magnetic element comprises a negative pole facing the array ofsensing coils and the second magnetic element comprises a positive polefacing the array of sensing coils.

Example 41—A surgical instrument, comprising a drive system thatcomprises a drive member movable between a first position and a secondposition during a drive stroke, and a magnetic member mounted to thedrive member. The surgical instrument further comprises a Hall effectsensor configured to detect the magnetic element throughout the entirerange of the drive stroke, and a controller in communication with theHall effect sensor.

Example 42—The surgical instrument of Example 41, further comprising ashaft and a wiring harness extending through the shaft, wherein the Halleffect sensor is integrated into the wiring harness.

Example 43—A surgical instrument, comprising a drive system thatcomprises a drive member movable between a first position, a secondposition, and a third position during a drive stroke. The drive systemfurther comprises a magnetic member mounted to the drive member. Thesurgical instrument further comprises a first Hall effect sensorconfigured to detect the magnetic element between the first position andthe second position but not beyond the second position, a second Halleffect sensor configured to detect the magnetic element between thesecond position and the third position but not before the secondposition, and a controller in communication with the first Hall effectsensor and the second Hall effect sensor.

Example 44—The surgical instrument of Example 43, further comprising ashaft and a wiring harness extending through the shaft, wherein thefirst Hall effect sensor and the second Hall effect sensor areintegrated into the wiring harness.

Example 45—A surgical instrument, comprising a drive system thatcomprises a drive member movable between a first position and a secondposition during a drive stroke, and a longitudinal array of magneticmembers mounted to the drive member. The surgical instrument furthercomprises a Hall effect sensor configured to detect the array ofmagnetic elements, and a controller in communication with the Halleffect sensor.

Example 46—The surgical instrument of Example 45, wherein the array ofmagnetic members comprises a first magnetic member and a second magneticmember, wherein the first magnetic member is positioned distally withrespect to the second magnetic member, and wherein the first magneticmember comprises a first polarity profile and the second magnetic membercomprises a second polarity profile that is different than the firstpolarity profile.

Example 47—The surgical instrument of Example 45, wherein the array ofmagnetic members comprises a plurality of distal magnetic members and aproximal-most magnetic member, wherein each the distal magnetic membercomprises a first polarity profile, and wherein the distal-most magneticmember comprises a second polarity profile which is different than thefirst polarity profile.

Example 48—The surgical instrument of Examples 45, 46, or 47, whereinthe drive system comprises an electric motor in communication with thecontroller, and wherein the controller is configured to slow theelectric motor when the Hall effect sensor detects the presence of thedistal-most magnetic element.

Example 49—The surgical instrument of Examples 45, 46, 47, or 48,further comprising a shaft and a wiring harness extending through theshaft, wherein the Hall effect sensor is integrated into the wiringharness.

Example 50—A surgical instrument, comprising a shaft, and a drive systemcomprising a drive member movable between a first position and a secondposition during a drive stroke, and a wiring harness extending in theshaft. The wiring harness comprises a first capacitive plate, a secondcapacitive plate, and a gap defined between the first capacitive plateand the capacitive plate. The drive member is movable between the firstcapacitive plate and the second capacitive plate during the drivestroke. The surgical instrument further comprises a controller incommunication with the first capacitive plate and the second capacitiveplate, wherein the controller is configured to track the position of thedrive member via the first capacitive plate and the second capacitiveplate.

Example 51—A surgical instrument, comprising a shaft, and a drive systemcomprising a drive member movable between a first position and a secondposition during a drive stroke, and a wiring harness extending in theshaft. The wiring harness comprises a first capacitive plate, and asecond capacitive plate, wherein the second capacitive plate ispositioned distally with respect to the first capacitive plate. Thesurgical instrument further comprises a controller in communication withthe first capacitive plate and the second capacitive plate, wherein thecontroller is configured to track the position of the drive member viathe first capacitive plate and the second capacitive plate.

Example 52—A surgical instrument, comprising a shaft, and a drive systemcomprising a drive member movable between a first position and a secondposition during a drive stroke, wherein the drive member comprises alight emitting diode configured to emit light. The surgical instrumentfurther comprises a wiring harness extending in the shaft comprising anoptical sensor, wherein the optical sensor is configured to detect theintensity of the light. The surgical instrument further comprises acontroller in communication with the optical sensor, wherein thecontroller is configured to track the position of the drive member bydata from the optical sensor.

Example 53—A surgical instrument, comprising a shaft, and a drive systemcomprising a drive member movable between a first position and a secondposition during a drive stroke, wherein the drive member comprises alongitudinal array of light emitting diodes configured to emit light.The surgical instrument further comprises a screen comprising anaperture extending therethrough, wherein the longitudinal array of lightemitting diodes is positioned on a first side of the screen. Thesurgical instrument further comprises a wiring harness extending in theshaft comprising an optical sensor positioned on a second side of thescreen, wherein the optical sensor is aligned with the aperture and isconfigured to detect the intensity of light emitted through theaperture. The surgical instrument further comprises a controller incommunication with the optical sensor, wherein the controller isconfigured to track the position of the drive member by data from theoptical sensor.

EXAMPLE SET 5

Example 1—A surgical instrument assembly, comprising a shaft, an endeffector attached to the shaft, and a sensing system positioned withinthe shaft. The sensing system is configured to detect a parameter of thesurgical instrument assembly, and detect a presence of outsideinterference that affects the parameter detection of the surgicalinstrument assembly.

Example 2—The surgical instrument assembly of Example 1, wherein thesensing system comprises a plurality of Hall effect sensors and a magnetconfigured to be sensed by the plurality of Hall effect sensors, andwherein the plurality of Hall effect sensors comprises a range ofexpected output values corresponding to the parameter.

Example 3—The surgical instrument assembly of Example 1, wherein thesensing system comprises a plurality of Hall effect sensors and aplurality of magnets configured to be sensed by the plurality of Halleffect sensors, and wherein the plurality of Hall effect sensorscomprises a range of expected output values corresponding to theparameter.

Example 4—A surgical instrument system, comprising a surgical instrumentassembly that comprises a shaft, an end effector attached to the shaft,and a sensing system positioned within the shaft. The sensing system isconfigured to detect a parameter of the surgical instrument assembly,and detect a presence of outside interference that affects the parameterdetection of the surgical instrument assembly. The surgical instrumentsystem further comprises a control circuit configured to receive asignal from the sensing system, determine if the received signal hasbeen altered by outside interference, and adjust the control program ifthe signal has been determined to have been altered by outsideinterference.

Example 5—A surgical instrument system, comprising a surgical instrumentassembly that comprises a motor, an actuation member configured to beactuated by the motor, and a shaft. The surgical instrument assemblyfurther comprises an end effector attached to the shaft, a first sensingsystem positioned within the shaft configured to monitor a parameter ofthe actuation member, and a second sensing system configured monitor aparameter of the motor. The surgical instrument system further comprisesa control circuit comprising a motor control program configured to runthe motor. The control circuit is configured to compare the monitoredparameter of the actuation member and the monitored parameter of themotor, and adjust the motor control program if the comparison of themonitored parameter of the actuation member and the monitored parameterof the motor does not comprise an expected relationship.

Example 6—A surgical instrument system, comprising a surgical instrumentcontrol interface comprising a first wireless communication module, anda first surgical instrument assembly configured to be attached to thesurgical instrument control interface, wherein the first surgicalinstrument assembly comprises a second wireless communication module.The surgical instrument system further comprises a second surgicalinstrument assembly configured to be attached to the surgical instrumentcontrol interface, wherein the second surgical instrument assemblycomprises a third wireless communication module. The surgical instrumentsystem further comprises a control circuit. The control circuit isconfigured to receive wireless communication signals from the secondwireless communication module and the third wireless communicationmodule prior to either of the first surgical instrument assembly or thesecond surgical instrument assembly being attached to the surgicalinstrument control interface. The control circuit is further configuredto alert a user of the identification of the first surgical instrumentassembly and the second surgical instrument assembly based on thereceived wireless communication signals.

Example 7—A surgical instrument system, comprising a surgical instrumentcontrol interface comprising an interface field detection sensor, and afirst surgical instrument assembly configured to be attached to thesurgical instrument control interface, wherein the first surgicalinstrument assembly comprises a first wireless communication module anda first field detection sensor. The surgical instrument system furthercomprising a second surgical instrument assembly configured to beattached to the surgical instrument control interface, wherein thesecond surgical instrument assembly comprises a second wirelesscommunication module and a second field detection sensor. The surgicalinstrument system further comprising a controller. The controller isconfigured to receive wireless communication signals from the firstwireless communication module containing data from the first fielddetection sensor and communication signals from the second wirelesscommunication module containing data from the second field detectionsensor. The controller is further configured to alert a user of theexistence of field interference with the surgical instrument systembased on the received wireless communication signals.

Example 8—The surgical instrument system of Example 7, wherein thecontroller is configured to assess whether the field interference isbeing generated by a source external to the surgical instrument system.

Example 9—The surgical instrument system of Examples 7 or 8, wherein thecontroller is configured to assess when the field interference isconstant and, when constant, discount the constant field interferencewhile operating the surgical instrument system.

Example 10—The surgical instrument system of Examples 7, 8, or 9,wherein the controller is configured to assess when the fieldinterference is stationary and, when stationary, discount the stationaryfield interference while operating the surgical instrument system.

Example 11—The surgical instrument system of Examples 7, 8, 9, or 10,wherein the controller is configured to assess when the fieldinterference is not constant and stationary and warn the user of thesurgical instrument system that one or more systems of the surgicalinstrument system may not function properly.

Example 12—The surgical instrument system of Example 11, wherein thecontroller is further configured to place the surgical instrument systemin a limp mode by limiting the operation of one or more systems.

Example 13—The surgical instrument system of Examples 11, or 12, whereinthe controller is further configured to place the surgical instrumentsystem in a limp mode by limiting the speed of one or more systems.

Example 14—The surgical instrument system of Examples 11, 12, or 13,wherein the controller is further configured to place the surgicalinstrument system in a limp mode by limiting the torque of one or moresystems.

Example 15—The surgical instrument system of Examples 11, 12, 13, or 14,wherein the controller is further configured to place the surgicalinstrument system in a limp mode by limiting the power of one or moresystems.

Example 16—The surgical instrument system of Examples 11, 12, 13, 14, or15, wherein the controller is further configured to place the surgicalinstrument system in a limp mode by preventing the operation of one ormore the systems.

Example 17—The surgical instrument system of Examples 11, 12, 13, 14,15, or 16, wherein the controller is further configured to place thesurgical instrument system in a limp mode by limiting the direction ofone or more systems.

Example 18—The surgical instrument system of Examples 7, 8, 9, 10, 11,12, 13, 14, 15, 16, or 17, wherein the controller is configured toassess whether the field interference is being generated by a sourceinternal to the surgical instrument system.

Example 19—The surgical instrument system of Examples 7, 8, 9, 10, 11,12, 13, 14, 15, 16, 17, or 18, wherein the controller is configured todetermine the origin of the field interference and reduce the fieldinterference below a threshold.

Example 20—A surgical instrument system, comprising a first Hall effectsensor, a second Hall effect sensor, and a controller. The controller isconfigured to receive signals from the first Hall effect sensor and thesecond Hall effect sensor, determine the presence of field interferencewith at least one of the first Hall effect sensor and the second Halleffect sensor, and alert a user of the existence of field interferencewith the surgical instrument system based on the signals.

Example 21—The surgical instrument system of Example 20, wherein thecontroller is configured to assess whether the field interference isbeing generated by a source external to the surgical instrument system.

Example 22—The surgical instrument system of Examples 20 or 21, whereinthe controller is configured to assess when the field interference isconstant and, when constant, discount the constant field interferencewhile operating the surgical instrument system.

Example 23—The surgical instrument system of Examples 20, 21, or 22,wherein the controller is configured to assess when the fieldinterference is stationary and, when stationary, discount the stationaryfield interference while operating the surgical instrument system.

Example 24—The surgical instrument system of Examples 20, 21, 22, or 23,wherein the controller is configured to assess when the fieldinterference is not constant and stationary and warn the user of thesurgical instrument system that one or more systems of the surgicalinstrument system may not function properly.

Example 25—The surgical instrument system of Example 24, wherein thecontroller is further configured to place the surgical instrument systemin a limp mode by limiting the operation of one or more systems.

Example 26—The surgical instrument system of Examples 24 or 25, whereinthe controller is further configured to place the surgical instrumentsystem in a limp mode by limiting the speed of one or more systems.

Example 27—The surgical instrument system of Examples 24, 25, or 26,wherein the controller is further configured to place the surgicalinstrument system in a limp mode by limiting the torque of one or moresystems.

Example 28—The surgical instrument system of Examples 24, 25, 26, or 27,wherein the controller is further configured to place the surgicalinstrument system in a limp mode by limiting the power of one or moresystems.

Example 29—The surgical instrument system of Examples 24, 25, 26, 27, or28, wherein the controller is further configured to place the surgicalinstrument system in a limp mode by preventing the operation of one ormore systems.

Example 30—The surgical instrument system of Examples 24, 25, 26, 27,28, or 29, wherein the controller is further configured to place thesurgical instrument system in a limp mode by limiting the direction ofone or more systems.

Example 31—The surgical instrument system of Examples 20, 21, 22, 23,24, 25, 26, 27, 28, 29, or 30, wherein the controller is configured toassess whether the field interference is being generated by a sourceinternal to the surgical instrument system.

Example 32—The surgical instrument system of Examples 20, 21, 22, 23,24, 25, 26, 27, 28, 29, 30, or 31, wherein the controller is configuredto determine the origin of the field interference and reduce the fieldinterference below a threshold.

Example 33—The surgical instrument system of Examples 20, 21, 22, 23,24, 25, 26, 27, 28, 29, 30, 31, or 32, further comprising a drive systemincluding a drive member, wherein the first Hall effect sensor isconfigured to detect the position of the drive member.

Example 34—The surgical instrument system of Example 33, wherein thesecond Hall effect sensor is configured to detect the position of thedrive member.

Example 35—The surgical instrument system of Example 33, wherein thesecond Hall effect sensor is dedicated to sensing the field interferenceand not the position of the drive member.

Example 36—The surgical instrument system of Examples 20, 21, 22, 23,24, 25, 26, 27, 28, 29, 30, 31 or, 32, wherein the first Hall effectsensor and the second Hall effect sensor are dedicated to detecting thefield interference and not the position of a drive member.

EXAMPLE SET 6

Example 1—A surgical instrument assembly, comprising a shaft, an endeffector attached to the shaft, and an actuation member positionedwithin the shaft. The surgical instrument assembly further comprises amotor configured to actuate the actuation member, an orientationdetection system configured to determine the orientation of the shaftrelative to the motor, and a control circuit configured to adjust theactuation of the motor based on the determined orientation of the shaftrelative to the motor.

Example 2—A surgical instrument assembly, comprising a shaft, an endeffector attached to the shaft, and an actuation member positionedwithin the shaft. The surgical instrument assembly further comprises amotor configured to actuate the actuation member; an orientationdetection system configured to determine the orientation of the endeffector relative to the motor, and a control circuit configured toadjust the actuation of the motor based on the determined orientation ofthe end effector relative to the motor.

Example 3—A surgical instrument system, comprising a housing interfacecomprising a motor, and a shaft assembly attachable to the housinginterface. The shaft assembly comprises a shaft, an end effectorattached to the shaft, an actuation member positioned within the shaft,and an orientation detection system configured to determine theorientation of the shaft relative to the housing interface. The surgicalinstrument system further comprises a control circuit comprising a motorcontrol program configured to run the motor, wherein the control circuitis configured to adjust the motor control program based on thedetermined orientation of the shaft relative to the housing interface.

Example 4—The surgical instrument system of Example 3, wherein thecontrol circuit is configured to adjust a rate of actuation of theactuation member.

Example 5—The surgical instrument system of Examples 3 or 4, wherein thecontrol circuit is configured to adjust a stroke length of the actuationmember.

Example 6—A surgical instrument system, comprising a handle comprising amotor and a trigger configured to actuate the motor, and a shaftassembly attachable to the handle. The shaft assembly comprises a shaft,an end effector attached to the shaft, and an actuation memberpositioned within the shaft. The surgical instrument system furthercomprises an orientation detection system configured to determine theorientation of the handle, and a control circuit configured to adjust aforce required to actuate the trigger based on the determinedorientation of the handle.

Example 7—The surgical instrument system of Example 6, wherein thecontrol circuit is configured to reduce the force required to actuatethe trigger when the handle is determined to be inverted.

Example 8—A surgical instrument system, comprising a housing. Thehousing comprises an attachment interface comprising a plurality of slipring contacts, wherein each slip ring contact comprises an interruptedconductor path. The housing further comprises a motor. The surgicalinstrument system further comprises a shaft assembly attachable to theattachment interface, wherein the shaft assembly is configured to berotated about a longitudinal shaft axis relative to the attachmentinterface. The shaft assembly comprises a proximal attachment portioncomprising electrical contacts configured to engage the slip ringcontacts when the shaft assembly is attached to the attachmentinterface. The shaft assembly further comprises a shaft, an end effectorattached to the shaft; and an actuation member positioned within theshaft. The surgical instrument system further comprises a controlcircuit. The control circuit is configured to monitor the position ofthe electrical contacts relative to the slip ring contacts, anddetermine the orientation of the shaft assembly based on the monitoredposition of the electrical contacts relative to the slip ring contacts.

Example 9—A surgical instrument system, comprising a surgical instrumentassembly that comprises a shaft, and an end effector attached to theshaft. The end effector comprises a first jaw, and a second jaw movablerelative to the first jaw. The surgical instrument system furthercomprises a control circuit. The control circuit is configured todetermine the orientation of the end effector relative to gravity, andadjust control motions applied to the end effector based on thedetermined orientation of the end effector relative to gravity.

Example 10—A surgical instrument system configured for use on a patient,wherein the surgical instrument system comprises a surgical instrumentassembly. The surgical instrument assembly comprises a shaft, and an endeffector attached to the shaft. The surgical instrument system furthercomprises a control circuit. The control circuit is configured todetermine the orientation of the patient, and adjust a control programof the surgical instrument assembly based on the determined orientationof the patient.

Example 11—A surgical instrument system configured for treating apatient, wherein the surgical instrument system comprises a surgicalinstrument. The surgical instrument comprises a shaft, and an endeffector extending from the shaft. The surgical instrument systemfurther comprises a control circuit. The control circuit is configuredto determine the orientation of the patient, determine the orientationof the surgical instrument, and adjust a control program of the surgicalinstrument assembly based on the determined orientation of the patientand the determined orientation of the surgical instrument.

Example 12—A surgical instrument system, comprising a surgicalinstrument. The surgical instrument comprises a handle, a shaft defininga longitudinal axis, and a rotation joint rotatably connecting the shaftto the handle, wherein the shaft is rotatable relative to the handleabout the longitudinal axis. The surgical instrument further comprisesan end effector extending from the shaft. The end effector comprises afirst jaw, and a second jaw movable relative to the first jaw. Thesurgical instrument system further comprises a control circuitconfigured to determine the orientation of the end effector relative togravity, and adjust control motions applied to the end effector based onthe determined orientation of the end effector relative to gravity.

Example 13—A surgical instrument system, comprising a surgicalinstrument. The surgical instrument comprises a shaft defining alongitudinal axis, and an end effector extending from the shaft. The endeffector comprises a first jaw, a second jaw movable relative to thefirst jaw about a closure joint, and an articulation joint, wherein thefirst jaw and the second jaw are articulatable laterally relative to thelongitudinal axis. The surgical instrument further comprises a rotationjoint rotatably connecting the end effector to the shaft, wherein theend effector is rotatable relative to the shaft about the longitudinalaxis. The surgical instrument system further comprises a controlcircuit. The control circuit is configured to determine the orientationof the end effector relative to gravity, and adjust control motionsapplied to the end effector based on the determined orientation of theend effector relative to gravity.

Example 14—A surgical instrument system, comprising a handle comprisinga motor and a trigger configured to actuate the motor, and a shaftextending from the handle. The shaft comprises a shaft, an end effectorattached to the shaft, and an actuation member. The surgical instrumentsystem further comprises an orientation detection system configured todetermine the orientation of the handle relative to gravity, and acontrol circuit configured to adjust a force required to actuate thetrigger based on the determined orientation of the handle.

Example 15—The surgical instrument system of Example 14, wherein thecontrol circuit is configured to reduce the force required to actuatethe trigger when the handle is determined to be inverted relative togravity.

Example 16—The surgical instrument system of Example 14, wherein thecontrol circuit is configured to increase the force required to actuatethe trigger when the handle is determined to be inverted relative togravity.

Example 17—A surgical instrument system, comprising a handle comprisinga motor and a trigger configured to actuate the motor, and a shaft. Theshaft comprises a shaft defining a longitudinal axis, an end effectorattached to the shaft, and an actuation member. The surgical instrumentsystem further comprises a rotation joint rotatably connecting the shaftto the handle such that the shaft is rotatable relative to the handleabout the longitudinal axis, an orientation detection system configuredto determine the orientation of the handle relative to the shaft, and acontrol circuit configured to adjust a force required to actuate thetrigger based on the determined orientation of the handle.

Example 18—The surgical instrument system of Example 17, wherein thecontrol circuit is configured to reduce the force required to actuatethe trigger when the handle is determined to be inverted relative to theshaft.

Example 19—The surgical instrument system of Example 17, wherein thecontrol circuit is configured to increase the force required to actuatethe trigger when the handle is determined to be inverted relative to theshaft.

EXAMPLE SET 7

Example 1—A surgical instrument system, comprising a surgical instrumentassembly. The surgical instrument assembly comprises a shaft, and an endeffector attached to the shaft. The surgical instrument system furthercomprises a control circuit configured to limit operation of thesurgical instrument assembly to a limited-capabilities state based on apredefined software configuration.

Example 2—The surgical instrument system of Example 1, wherein thecontrol circuit is configured to receive an input from a user to unlocka full-capabilities state of the surgical instrument assembly.

Example 3—The surgical instrument system of Examples 1 or 2, wherein thelimited-capabilities state comprises limiting an actuation-membersensing system to a reduced functional state.

Example 4—A surgical instrument system, comprising a surgical instrumentassembly that comprises a shaft, and an end effector attached to theshaft. The surgical instrument system further comprises a controlcircuit. The control circuit is configured to determine alimited-capabilities operating mode, and recommend thelimited-capabilities operating mode to a user of the surgical instrumentassembly.

Example 5—A surgical instrument system, comprising a surgical instrumentassembly. The surgical instrument assembly comprises a shaft, an endeffector attached to the shaft, and an electro-mechanical system. Thesurgical instrument system that comprises a control circuit configuredto limit a functional range of the electro-mechanical system based on alevel of available power to the surgical instrument assembly.

Example 6—A surgical instrument system, comprising a surgicalcommunications hub and a surgical instrument. The surgical instrumentcomprises a controller, a first set of firmware, and a communicationssystem. The communications system is configured to communicate with thesurgical communications hub, wherein the first set of firmware issuitable for the surgical instrument to perform a first surgicaltechnique. The controller is selectively operable by the user of thesurgical instrument system to upload a second set of firmware from thesurgical communications hub that makes the surgical instrument suitableto perform a second surgical technique which is different than the firstsurgical technique.

Example 7—The surgical instrument system of Example 6, wherein thesurgical instrument comprises a shaft, an end effector, an articulationjoint rotatably connecting the end effector to the shaft, and anarticulation drive system. The articulation drive system comprises anarticulation motor in communication with the controller. The controlleris configured to move the end effector through a first articulationrange when the controller is using the first set of firmware. Thecontroller is configured to move the end effector through a secondarticulation range when the controller is using the second set offirmware. The first articulation range is less than the secondarticulation range.

Example 8—The surgical instrument system of Example 6, wherein thesurgical instrument comprises a shaft, an end effector, an articulationjoint rotatably connecting the end effector to the shaft, and anarticulation drive system. The articulation drive system comprises anarticulation motor in communication with the controller. The controlleris configured to move the end effector through a first articulationrange when the controller is using the first set of firmware. Thecontroller is configured to move the end effector through a secondarticulation range when the controller is using the second set offirmware. The first articulation range is greater than the secondarticulation range.

Example 9—The surgical instrument system of Example 6, wherein thesurgical instrument comprises a shaft, an end effector, and a firstarticulation joint defining a first articulation axis. The surgicalinstrument further comprises a second articulation joint defining asecond articulation axis, a first articulation drive system comprising afirst articulation motor in communication with the controller, and asecond articulation drive system comprising a second articulation motorin communication with the controller. The controller configured to usethe first articulation drive system but not the second articulationdrive system when the controller is using the first set of firmware. Thecontroller configured to use the first articulation drive system and thesecond articulation drive system when the controller is using the secondset of firmware.

Example 10—The surgical instrument system of Example 6, wherein thesurgical instrument comprises a shaft, an end effector, and a firstarticulation joint defining a first articulation axis. The surgicalinstrument further comprises a second articulation joint defining asecond articulation axis, a first articulation drive system comprising afirst articulation motor in communication with the controller, and asecond articulation drive system comprising a second articulation motorin communication with the controller. The controller is configured touse the first articulation drive system and the second articulationdrive system when the controller is using the first set of firmware. Thecontroller is configured to use the first articulation drive system butnot the second articulation drive system when the controller is usingthe second set of firmware.

Example 11—The surgical instrument system of Example 6, wherein thesurgical instrument comprises a shaft, and an end effector. The endeffector comprises a first jaw and a second jaw, wherein the first jawis rotatable relative to the second jaw. The surgical instrument furthercomprises a drive system configured to move the first jaw relative tothe second jaw. The drive system is in communication with thecontroller. The controller is configured to move the first jaw through afirst range of motion when using the first set of firmware. Thecontroller is configured to move the first jaw through a second range ofmotion when using the second set of firmware. The second range of motionis larger than and overlaps the first range of motion.

Example 12—The surgical instrument system of Example 6, wherein thesurgical instrument comprises a shaft, and an end effector. The endeffector comprises a first jaw and a second jaw, wherein the first jawis rotatable relative to the second jaw. The surgical instrument furthercomprises a drive system configured to move the first jaw relative tothe second jaw. The drive system is in communication with thecontroller. The controller is configured to move the first jaw through afirst range of motion when using the first set of firmware. Thecontroller is configured to move the first jaw through a second range ofmotion when using the second set of firmware. The first range of motionis larger than and overlaps the second range of motion.

Example 13—The surgical instrument system of Examples 6, 7, 8, 9, 10,11, or 12, wherein the surgical instrument comprises a drive systemincluding an electric motor in communication with the controller and apower source. The controller limits the power supplied to the electricmotor from the power source to a first power limit when using the firstset of firmware. The controller limits the power supplied to theelectric motor from the power source to a second power limit when usingthe second set of firmware. The second power limit is higher than thefirst power limit.

Example 14—The surgical instrument system of Examples 6, 7, 8, 9, 10,11, or 12, wherein the surgical instrument comprises a drive systemincluding an electric motor in communication with the controller and apower source. The controller limits the power supplied to the electricmotor from the power source to a first power limit when using the firstset of firmware. The controller limits the power supplied to theelectric motor from the power source to a second power limit when usingthe second set of firmware. The second power limit is lower than thefirst power limit.

Example 15—The surgical instrument system of Examples 6, 7, 8, 9, 10,11, 12, 13, or 14, wherein the surgical instrument comprises an energydelivery system in communication with the controller and a power source.The controller limits the power supplied to the energy delivery systemfrom the power source to a first power limit when using the first set offirmware. The controller limits the power supplied to the energydelivery system from the power source to a second power limit when usingthe second set of firmware. The second power limit is higher than thefirst power limit.

Example 16—The surgical instrument system of Examples 6, 7, 8, 9, 10,11, 12, 13, or 14, wherein the surgical instrument comprises an energydelivery system in communication with the controller and a power source.The controller limits the power supplied to the energy delivery systemfrom the power source to a first power limit when using the first set offirmware. The controller limits the power supplied to the energydelivery system from the power source to a second power limit when usingthe second set of firmware. The second power limit is lower than thefirst power limit.

Example 17—The surgical instrument system of Examples 6, 7, 8, 9, 10,11, 12, 13, 14, 15, or 16 wherein the controller powers thecommunications system of the surgical instrument to have a first rangewhen using the first set of firmware, wherein the controller powers thecommunications system of the surgical instrument to have a second rangewhen using the second set of firmware, and wherein the second range islonger than the first range.

Example 18—The surgical instrument system of Examples 6, 7, 8, 9, 10,11, 12, 13, 14, 15, or 16, wherein the controller powers thecommunications system of the surgical instrument to have a first rangewhen using the first set of firmware, wherein the controller powers thecommunications system of the surgical instrument to have a second rangewhen using the second set of firmware, and wherein the second range isshorter than the first range.

Example 19—The surgical instrument system of Examples 6, 7, 8, 9, 10,11, 12, 13, 14, 15, 16, 17, or 18, wherein the surgical communicationshub comprises a payment protocol that requires a payment beforedelivering the second set of firmware to the surgical instrument.

Example 20—The surgical instrument system of Examples 6, 7, 8, 9, 10,11, 12, 13, 14, 15, 16, 17, 18, or 19, wherein the controller isconfigured to at least one of override or limit changes downloaded tothe surgical instrument based on the sensed performance of the surgicalinstrument.

EXAMPLE SET 8

Example 1—A surgical instrument system, comprising a surgical instrumentassembly configured to be attached to an actuation interface. Thesurgical instrument assembly comprises a shaft, an end effector attachedto the shaft, and a memory. The surgical instrument system furthercomprises a control circuit configured to run the actuation interface.The control circuit is configured to receive calibration parameters fromthe memory based on the surgical instrument assembly, and update a motorcontrol program based on the received calibration parameters.

Example 2—A surgical instrument system, comprising a surgical instrumentassembly configured to be attached to an actuation interface. Thesurgical instrument assembly comprises a shaft, an end effector attachedto the shaft, and a memory. The surgical instrument system furthercomprises a control circuit configured to run the actuation interface.The control circuit is configured to receive component identifiers fromthe memory based on the surgical instrument assembly, and determine amotor control program based on the received component identifiers.

Example 3—A surgical instrument system, comprising a surgical instrumentassembly configured to be attached to an actuation interface. Thesurgical instrument assembly comprises a modular shaft comprising afirst memory, and a modular end effector. The modular end effectorcomprises a second memory, wherein the modular end effector isconfigured to be attached to shaft. The modular end effector furthercomprises a control circuit configured to run the actuation interface.The control circuit is configured to receive a first component-specificinformation from the first memory and a second component-specificinformation from the second memory, and determine a motor controlprogram based on the received first component-specific information andthe received second component-specific information.

Example 4—A surgical instrument system, comprising a surgical instrumentassembly comprising a plurality of sub-systems, and a control interface.The control interface comprises an attachment portion, wherein thesurgical instrument assembly is configured to be attached to theattachment portion. The control interface further comprises one or moremotors configured to actuate the plurality of sub-systems. The surgicalinstrument system further comprises a control circuit. The controlcircuit is configured to identify each sub-system of the surgicalinstrument assembly when the surgical instrument assembly is attached tothe attachment portion, actuate each sub-system through a test stroke,and optimize one or more control programs according to the test stroke.

Example 5—A surgical instrument system, comprising a surgical instrumentassembly comprising a plurality of sub-systems, and a control interface.The control interface comprises an attachment portion, wherein thesurgical instrument assembly is configured to be attached to theattachment portion. The control interface further comprises one or moremotors configured to actuate the plurality of sub-systems. The surgicalinstrument system further comprises a control circuit. The controlcircuit is configured to identify each sub-system of the surgicalinstrument assembly when the surgical instrument assembly is attached tothe attachment portion, actuate each sub-system through a test stroke,and generates one or more control programs according to the test stroke.

Example 6—The surgical instrument system of Example 5, wherein thecontrol circuit is further configured to compare the test stroke toactuations of surgical instrument assemblies previously attached to thecontrol interface, and determine if the control interface is causingvariation in actuations and if the surgical instrument assembly iscausing variation in actuation.

Example 7—A surgical instrument system, comprising a surgical instrumentassembly. The surgical instrument assembly comprises a shaft, an endeffector attached to the shaft, a drive system positioned within theshaft, and an onboard memory configured to store identification datacorresponding to the drive system. The surgical instrument systemfurther comprises a control circuit. The control circuit is configuredto access the identification data stored on the onboard memory, identifythe surgical instrument assembly based on the accessed identificationdata, and determine a motor control program to actuate the surgicalinstrument assembly based on the identified surgical instrumentassembly.

Example 8—A surgical instrument system, comprising a handle. The handlecomprises a frame, a first drive system including a first drive motor,and a second drive system including a second drive motor. The handlefurther comprises a control system in communication with the first drivemotor and the second drive motor, and an attachment sensor incommunication with the control system. The surgical instrument systemfurther comprises a shaft attachable to the handle. The shaft comprisesa connector portion releaseably mountable to the frame, a first drivemember comprising a first proximal connector that is coupled to thefirst drive system when the shaft is attached to the handle, and asecond drive member comprising a second proximal connector that iscoupled to the second drive system when the shaft is attached to thehandle. The control system is configured to move the first drive memberthrough a first test stroke when the shaft is attached to the handle toassess at least one of slop, backlash, friction loss, stroke variation,and motor stall in the first drive system and the first drive member.The control system is configured to move the second drive member througha second test stroke when the shaft is attached to the handle to assessat least one of slop, backlash, friction loss, stroke variation, andmotor stall in the second drive system and the second drive member.

Example 9—The surgical instrument system of Example 8, wherein thecontroller is configured to alter the motor control algorithm forcontrolling the first drive motor based on the controller's assessmentof the first drive system and the first drive member, and wherein thecontroller is configured to alter the motor control algorithm forcontrolling the second drive motor based on the controller's assessmentof the second drive system and the second drive member.

Example 10—A surgical instrument system, comprising a surgicalinstrument. The surgical instrument comprises an actuation interfacecomprising an interface memory device, a drive system comprising anelectric motor, a motor control program, and a shaft releaseablyattachable to the actuation interface. The shaft comprises a controlcircuit configured to access the interface memory device when the shaftis attached to the actuation interface to obtain data regarding theactuation interface. The shaft further comprises a shaft memory devicein communication with the control circuit, and a communications circuitin communication with the control circuit. The surgical instrumentsystem further comprises a surgical hub configured to communicate withthe control circuit and a remote server. The surgical hub is configuredto receive data from the interface memory device and the shaft memorydevice and transmit the data to the remote server to determine changesto the motor control program that will improve the operation of thesurgical instrument. The control circuit is configured to update themotor control program based on the changes.

Example 11—The surgical instrument system of Example 10, wherein thedata includes an identification number of the actuation interface and anidentification number of the shaft.

Example 12—The surgical instrument system of Examples 10 or 11, whereinthe data includes a manufacturing date of the actuation interface and amanufacturing date of the shaft.

Example 13—The surgical instrument system of Examples 10, 11, or 12,wherein the data includes a manufacturing site of the actuationinterface and a manufacturing site of the shaft.

Example 14—The surgical instrument system of Examples 10, 11, 12, or 13,wherein the data is used to evaluate the tolerances of the drive systemand a drive member of the shaft engaged with the drive system toestimate the stroke variation of the drive member.

Example 15—The surgical instrument system of Example 14, wherein theserver is configured to store the tolerance evaluation, stroke variationestimate, and motor control program changes.

Example 16—The surgical instrument system of Examples 10, 11, 12, 13,14, or 15, wherein the server is configured to transmit the motorcontrol program changes to other actuation interface and shaft pairingsthat have the same data.

Example 17—The surgical instrument system of Examples 10, 11, 12, 13,14, 15, or 16, wherein the server is configured to transmit the motorcontrol program changes to other actuation interface and shaft pairingsthat have the same identification numbers.

Example 18—The surgical instrument system of Examples 10, 11, 12, 13,14, 15, 16, or 17, wherein the shaft identification number is stored onan RFID tag on the shaft and the actuation interface identificationnumber is stored on an RFID tag on the actuation interface.

Example 19—The surgical instrument system of Examples 10, 11, 12, 13,14, 15, 16, 17, or 18, wherein at least one of the actuation interfaceand the shaft comprises a lockout configured to limit the operation ofthe drive member, and wherein the controller is configured to actuatethe lockout if the stroke variation estimate is outside of an acceptablerange.

Example 20—The surgical instrument system of Examples 10, 11, 12, 13,14, 15, 16, 17, 18, or 19, further comprising a lockout overrideconfigured to delimit the operation of the drive member.

Example 21—The surgical instrument system of Examples 10, 11, 12, 13,14, 15, 16, 17, 18, 19, or 20, wherein the controller is configured tomonitor the actual stroke of the drive member, assess the actual strokevariation of the drive member, compare the actual stroke variation tothe stroke variation estimate, and transmit the actual stroke variationto the surgical hub. The surgical hub is configured to transmit theactual stroke variation to the remote server. The remote server isconfigured to revise the stroke variation estimate based on the actualstroke variation.

Any patent application, patent, non-patent publication, or otherdisclosure material referred to in this specification and/or listed inany Application Data Sheet is incorporated by reference herein, to theextent that the incorporated materials is not inconsistent herewith. Assuch, and to the extent necessary, the disclosure as explicitly setforth herein supersedes any conflicting material incorporated herein byreference. Any material, or portion thereof, that is said to beincorporated by reference herein, but which conflicts with existingdefinitions, statements, or other disclosure material set forth hereinwill only be incorporated to the extent that no conflict arises betweenthat incorporated material and the existing disclosure material.

What is claimed is:
 1. A surgical instrument assembly, comprising: ashaft; an end effector attached to said shaft; and a sensing systempositioned within said shaft, wherein said sensing system is configuredto: detect a parameter of said surgical instrument assembly; and detecta presence of outside interference that affects the parameter detectionof said surgical instrument assembly.
 2. The surgical instrumentassembly of claim 1, wherein said sensing system comprises a pluralityof Hall effect sensors and a magnet configured to be sensed by saidplurality of Hall effect sensors, and wherein said plurality of Halleffect sensors comprises a range of expected output values correspondingto said parameter.
 3. The surgical instrument assembly of claim 1,wherein said sensing system comprises a plurality of Hall effect sensorsand a plurality of magnets configured to be sensed by said plurality ofHall effect sensors, and wherein said plurality of Hall effect sensorscomprises a range of expected output values corresponding to saidparameter.
 4. A surgical instrument system, comprising: a surgicalinstrument assembly, comprising: a shaft; an end effector attached tosaid shaft; and a sensing system positioned within said shaft, whereinsaid sensing system is configured to: detect a parameter of saidsurgical instrument assembly; and detect a presence of outsideinterference that affects the parameter detection of said surgicalinstrument assembly; and a control circuit configured to: receive asignal from said sensing system; determine if said received signal hasbeen altered by outside interference; adjust said control program ifsaid signal has been determined to have been altered by outsideinterference.
 5. A surgical instrument system, comprising: a surgicalinstrument control interface comprising an interface field detectionsensor; a first surgical instrument assembly configured to be attachedto said surgical instrument control interface, wherein said firstsurgical instrument assembly comprises a first wireless communicationmodule and a first field detection sensor; a second surgical instrumentassembly configured to be attached to said surgical instrument controlinterface, wherein said second surgical instrument assembly comprises asecond wireless communication module and a second field detectionsensor; and a controller configured to: receive wireless communicationsignals from said first wireless communication module containing datafrom said first field detection sensor and communication signals fromsaid second wireless communication module containing data from saidsecond field detection sensor; and alert a user of the existence offield interference with said surgical instrument system based on saidreceived wireless communication signals.
 6. The surgical instrumentsystem of claim 5, wherein said controller is configured to assesswhether said field interference is being generated by a source externalto said surgical instrument system.
 7. The surgical instrument system ofclaim 5, wherein said controller is configured to assess when said fieldinterference is constant and, when constant, discount the constant fieldinterference while operating said surgical instrument system.
 8. Thesurgical instrument system of claim 5, wherein said controller isconfigured to assess when said field interference is stationary and,when stationary, discount the stationary field interference whileoperating said surgical instrument system.
 9. The surgical instrumentsystem of claim 5, wherein said controller is configured to assess whensaid field interference is not constant and stationary and warn the userof the surgical instrument system that one or more systems of thesurgical instrument system may not function properly.
 10. The surgicalinstrument system of claim 9, wherein said controller is furtherconfigured to place said surgical instrument system in a limp mode bylimiting the operation of one or more said systems.
 11. The surgicalinstrument system of claim 9, wherein said controller is furtherconfigured to place said surgical instrument system in a limp mode bylimiting the speed of one or more said systems.
 12. The surgicalinstrument system of claim 9, wherein said controller is furtherconfigured to place said surgical instrument system in a limp mode bylimiting the torque of one or more said systems.
 13. The surgicalinstrument system of claim 9, wherein said controller is furtherconfigured to place said surgical instrument system in a limp mode bylimiting the power of one or more said systems.
 14. The surgicalinstrument system of claim 9, wherein said controller is furtherconfigured to place said surgical instrument system in a limp mode bypreventing the operation of one or more said systems.
 15. The surgicalinstrument system of claim 9, wherein said controller is furtherconfigured to place said surgical instrument system in a limp mode bylimiting the direction of one or more said systems.
 16. The surgicalinstrument system of claim 5, wherein said controller is configured toassess whether said field interference is being generated by a sourceinternal to said surgical instrument system.
 17. The surgical instrumentsystem of claim 16, wherein said controller is configured to determinethe origin of said field interference and reduce said field interferencebelow a threshold.